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Complete Course in Astrobiology Edited by Gerda Horneck and Petra Rettberg

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Page 1: Complete Course in Astrobiology (Physics Textbook)

Complete Course in Astrobiology

Edited by

Gerda Horneck and Petra Rettberg

Page 2: Complete Course in Astrobiology (Physics Textbook)

Each generation has its unique needs and aspirations. When Charles Wiley firstopened his small printing shop in lower Manhattan in 1807, it was a generationof boundless potential searching for an identity. And we were there, helping todefine a new American literary tradition. Over half a century later, in the midstof the Second Industrial Revolution, it was a generation focused on buildingthe future. Once again, we were there, supplying the critical scientific, technical,and engineering knowledge that helped frame the world. Throughout the 20thCentury, and into the new millennium, nations began to reach out beyond theirown borders and a new international community was born. Wiley was there, ex-panding its operations around the world to enable a global exchange of ideas,opinions, and know-how.

For 200 years, Wiley has been an integral part of each generation’s journey,enabling the flow of information and understanding necessary to meet theirneeds and fulfill their aspirations. Today, bold new technologies are changingthe way we live and learn. Wiley will be there, providing you the must-haveknowledge you need to imagine new worlds, new possibilities, and new oppor-tunities.

Generations come and go, but you can always count on Wiley to provide youthe knowledge you need, when and where you need it!

William J. Pesce Peter Booth WileyPresident and Chief Executive Officer Chairman of the Board

1807–2007 Knowledge for Generations

Page 3: Complete Course in Astrobiology (Physics Textbook)

Complete Course in Astrobiology

Edited byGerda Horneck and Petra Rettberg

Page 4: Complete Course in Astrobiology (Physics Textbook)

The Editors

Dr. Gerda HorneckDLRInst. of Aerospace Medicine51170 Kçln

Dr. Petra RettbergDLRInst. of Aerospace Medicine51147 Kçln

Cover Picture

Picture courtesy of ESO(The European Southern Observatory)

L All books published by Wiley-VCH are carefully pro-duced. Nevertheless, authors, editors, and publisherdo not warrant the information contained in thesebooks, including this book, to be free of errors.Readers are advised to keep in mind that statements,data, illustrations, procedural details or other itemsmay inadvertently be inaccurate.

Library of Congress Card No.:applied for

British Library Cataloguing-in-Publication DataA catalogue record for this book is available from theBritish Library.

Bibliographic information published bythe Deutsche NationalbibliothekDie Deutsche Nationalbibliothek lists this publicationin the Deutsche Nationalbibliografie; detailed biblio-graphic data are available in the Internet at<http://dnb.d-nb.de>.

� 2007 WILEY-VCH Verlag GmbH & Co. KGaA,Weinheim

All rights reserved (including those of translationinto other languages). No part of this book maybe reproduced in any form – by photoprinting,microfilm, or any other means – nor transmitted ortranslated into a machine language without writtenpermission from the publishers.Registered names, trademarks, etc. used in this book,even when not specifically marked as such, are notto be considered unprotected by law.

Typesetting Dçrr + Schiller GmbH, StuttgartPrinting betz-Druck GmbH, DarmstadtBinding Litges & Dopf Buchbinderei GmbH,

Heppenheim

Printed in the Federal Republic of GermanyPrinted on acid-free paper

ISBN: 978-3-527-40660-9

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Table of Contents

1 Astrobiology: From the Origin of Life on Earth to Life in the UniverseAndr� Brack

1.1 General Aspects of Astrobiology 11.1.1 Historical Milestones 11.1.2 Searching for Emerging Life 31.1.3 The Role of Water 41.1.4 The Physicochemical Features of Carbon-based Life 41.1.5 Clays as Possible Primitive Robots 61.2 Reconstructing Life in a Test Tube 71.2.1 The Quest for Organic Molecules 71.2.1.1 Terrestrial Production 71.2.1.2 Delivery of Extraterrestrial Organic Molecules 81.2.2 Space Experiments 101.2.3 Attempts to Recreate Life in a Test Tube 111.2.4 A Primitive Life Simpler than a Cell? 131.3 The Search for Traces of Primitive Life 141.3.1 Microfossils 141.3.2 Oldest Sedimentary Rocks 151.4 The Search for Life in the Solar System 151.4.1 Planet Mars and the SNC Meteorites 151.4.2 Jupiter’s Moon Europa 171.4.3 Saturn’s Moon Titan 181.5 The Search for Life Beyond the Solar System 191.5.1 The Search for Rocky Earthlike Exoplanets 191.5.2 Detecting Extrasolar Life 201.6 Conclusions 201.7 Further Reading 211.7.1 Books and Articles in Books 211.7.2 Articles in Journals 211.7.3 Web Sites 22

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Complete Course in Astrobiology. Edited by Gerda Horneck and Petra RettbergCopyright � 2007 WILEY-VCH Verlag GmbH & Co. KGaA, WeinheimISBN: 978-3-527-40660-9

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2 From the Big Bang to the Molecules of LifeHarry J. Lehto

2.1 Building Blocks of Life 232.2 Big Bang: Formation of H and He 252.3 First Stars: Formation of Small Amounts of C, O, N, S and P and

Other Heavy Elements 282.4 Normal Modern Stars, Bulk Formation of C, O, N, S, P and Other

Heavy Elements 292.5 The First Molecules (CO and H2O) 352.6 Interstellar Matter 352.6.1 Interstellar Clouds 372.6.2 Interstellar Grains 392.6.2.1 Formation 392.6.2.2 Observed Properties 402.6.3 Ices 412.6.4 Molecules in the Gas Phase 422.6.4.1 Observed Properties 422.6.4.2 Formation of H2 432.6.4.3 Formation of CO and H2O 442.7 Generation of Stars: Formation of the Sun and Planets 442.7.1 Accretion Disk of the Sun 442.7.2 Formation of the Earth 462.7.3 Early Rain ofMeteorites, Comets, Asteroids, and PrebioticMolecules 472.7.4 D/H Ratio and Oceans 492.8 Further Reading 512.8.1 Books or Articles in Books 512.8.2 Articles in Journals 512.8.3 Web Sites 532.9 Questions for Students 53

3 Basic Prebiotic ChemistryHerv� Cottin

3.1 Key Molecules of Life 553.1.1 Dismantling the Robots 563.1.2 Proteins and Amino Acids 583.1.3 DNA, RNA, and Their Building Blocks 603.1.4 First “Prebiotic Robot” 633.2 Historical Milestones 633.3 Sources of Prebiotic Organic Molecules 693.3.1 Endogenous Sources of Organic Molecules 693.3.1.1 Atmospheric Syntheses 693.3.1.2 Hydrothermal Vents 703.3.2 Exogenous Delivery of Organic Molecules 713.3.2.1 Comets 713.3.2.2 Meteorites 73

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3.3.2.3 Micrometeorites 743.3.3 Relative Contribution of the Different Sources 743.4 From Simple to Slightly More Complex Compounds 753.4.1 Synthesis of Amino Acids 753.4.2 Synthesis of Purine and Pyrimidine Bases 763.4.3 Synthesis of Sugars 783.4.4 Synthesis of Polymers 803.5 Conclusions 813.6 Further Reading 823.6.1 Books or Articles in Books 823.6.2 Articles in Journals 823.7 Questions for Students 833.7.1 Basic-level Questions 833.7.2 Advanced-level Questions 83

4 From Molecular Evolution to Cellular LifeKirsi Lehto

4.1 History of Life at Its Beginnings 854.2 Life as It Is Known 884.2.1 The Phylogenetic Tree of Life 884.2.2 Life is Cellular, Happens in Liquid Water, and Is Based on

Genetic Information 884.2.2.1 Genetic Information 924.2.2.2 The Genetic Code and Its Expression 944.3 Last Universal Common Ancestor (LUCA) 964.3.1 Containment in a Cell Membrane 974.3.2 Genes and Their Expression 994.3.3 Hypothetical Structure of the LUCA Genome 1034.4 “Life” in the RNA–Protein World: Issues and Possible Solutions 1054.4.1 Evolutionary Solutions 1064.4.2 Solutions Found in the Viral World 1074.5 “Life” Before the Appearance of the Progenote 1084.5.1 The Breakthrough Organism and the RNA–Protein World 1084.5.2 Primitive Translation Machinery 1084.5.3 Origin of Ribosomes 1094.6 The RNA World 1114.6.1 Origin of the RNA World 1134.6.1.1 Prebiotic Assembly of Polymers 1134.6.1.2 The Building Blocks of the RNA World 1144.6.1.3 Where Could the RNA World Exist and Function? 1154.7 Beginning of Life 1174.8 Further Reading 1184.8.1 Books 1184.8.2 Articles in Journals 1184.9 Questions for Students 120

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5 Extremophiles, the Physicochemical Limits of Life (Growth and Survival)Helga Stan-Lotter

5.1 A Brief History of Life on Earth 1215.1.1 Early Earth and Microfossils 1215.1.2 Prokaryotes, Eukaryotes, and the Tree of Life 1235.1.3 Some Characteristics of Bacteria and Archaea 1265.1.3.1 Cell Walls, Envelopes, and Shape 1265.1.3.2 Lipids and Membranes 1275.2 Extremophiles and Extreme Environments 1275.2.1 Growth versus Survival 1295.2.2 The Search for Life on Mars: The Viking Mission 1305.2.3 Temperature Ranges for Microorganisms 1325.2.4 High-temperature Environments 1335.2.4.1 Geography and Isolates 1335.2.4.2 Molecular Properties of Hyperthermophiles 1365.2.4.3 Early Evolution and Hyperthermophiles 1375.2.4.4 Applications 1385.2.5 Low-temperature Environments 1385.2.5.1 Geography and Isolates 1385.2.5.2 Molecular Adaptations 1395.2.6 Barophiles or Piezophiles 1405.2.7 High-salt Environments 1405.2.7.1 Hypersaline Environments and Isolates 1405.2.7.2 Viable Haloarchaea from Rock Salt 1415.2.7.3 Molecular Mechanisms 1425.2.7.4 Extraterrestrial Halite 1435.2.8 Subterranean Environments 1445.2.9 Radiation 1455.3 Microbial Survival of Extreme Conditions 1465.4 Conclusions 1485.5 Further Reading 1495.5.1 Books or Articles in Books 1495.5.2 Articles in Journals 1495.5.3 Web Sites 1505.6 Questions for Students 150

6 HabitabilityCharles S. Cockell

6.1 A Brief History of the Assessment of Habitability 1516.2 What Determines Habitability? 1546.3 Uninhabited Habitable Worlds 1566.4 Factors Determining Habitability 1566.4.1 Habitability and Temperature 1566.4.2 Habitability and Energy 1606.4.3 Other Factors that Determine Habitability 164

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6.5 A Postulate for Habitability 1656.5.1 Assumptions about the Habitat 1676.5.2 Assumptions on Life 1676.5.3 Attempt to Formulate a Habitability Postulate 1676.6 Some Test Cases for Habitability 1696.6.1 Test Case One: Life on Venus 1696.6.2 Test Case Two: Life on the Early Earth 1716.6.3 R�sum� of the Two Test Cases 1736.7 Conclusions 1736.8 Further Reading 1746.8.1 Books and Articles in Books 1746.8.2 Articles in Journals 1746.9 Questions for Students 176

7 Astrodynamics and Technological Aspects of Astrobiology Missionsin Our Solar SystemStefanos Fasoulas and Tino Schmiel

7.1 Introduction 1797.2 The Rocket Equation 1807.2.1 Single-staged Rockets 1807.2.2 Multiple-staged Rockets 1837.3 Orbital Mechanics and Astrodynamics 1847.3.1 Some Historical Notes 1847.3.2 The Energy Conservation Equation 1877.3.3 Some Typical Velocities 1887.4 Orbital Maneuvers 1907.4.1 High-thrust Maneuvers 1907.4.2 Low-thrust Maneuvers 1927.4.3 Gravity-assist Maneuvers 1937.5 Example: Missions to Mars 1957.6 Further Reading 2007.7 Questions for Students 200

8 Astrobiology of the Terrestrial Planets, with Emphasis on MarsMonica M. Grady

8.1 The Solar System 2038.2 Terrestrial Planets 2068.2.1 Mercury 2068.2.2 Venus 2078.2.3 Earth 2088.2.4 Mars 2088.2.4.1 Observing Mars 2088.2.4.2 Evidence for Water 2108.2.4.3 Evidence of Heat 2138.2.5 Meteorites from Mars 213

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8.2.5.1 Why from Mars? 2138.2.5.2 What can we Learn About Mars from Martian Meteorites? 2168.2.5.3 Microfossils in a Martian Meteorite? 2188.2.6 Can We Detect Signatures of Life on Mars? 2198.2.7 Conclusions: Life Beyond Earth? 2208.3 Further Reading 2208.3.1 Concerning Planetary Formation and Chronology 2208.3.2 Concerning Recent Results from Mars 2218.3.3 Concerning Terrestrial and Martian Microfossils 2218.3.4 Concerning Meteorites from Mars 2218.4 Questions for Students 222

9 Astrobiology of Saturn’s Moon TitanFranÅois Raulin

9.1 Extraterrestrial Bodies of Astrobiological Interest 2239.2 Some Historical Milestones in the Exploration of Titan 2259.3 General Properties, Formation and Internal Structure of Titan 2269.3.1 Main Properties 2269.3.2 Models of Formation and Internal Structure 2279.4 Atmosphere and Surface of Titan 2299.4.1 Theoretical Modeling of Titan’s Atmosphere 2299.4.2 Experimental Approach 2339.4.3 Observational Approach 2369.5 Astrobiological Aspects of Titan 2419.5.1 Analogies with Planet Earth 2419.5.2 Organic Chemistry 2429.5.3 Life on Titan? 2469.6 Outlook: Astrobiology and Future Exploration of Titan 2479.7 Further Reading 2499.7.1 Books and Articles in Books 2499.7.2 Articles in Journals 2509.7.3 Web Sites 2509.8 Questions for Students 251

10 Jupiter’s Moon Europa: Geology and HabitabilityChristophe Sotin and Daniel Prieur

10.1 A Short Survey of the Past Exploration of Europa 25310.2 Geology of the Moon Europa 25510.2.1 Surface Features 25510.2.2 Composition of the Surface 25710.3 Internal Structure of the Moon Europa 25810.4 Models of Evolution of the Moon Europa 26010.5 Astrobiological Considerations about Possibilities for Life

on the Moon Europa 26310.6 Summary and Conclusions 267

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10.7 Outlook and Plans for Future Missions 26810.8 Further Reading 26910.8.1 Books and Articles in Books 26910.8.2 Articles in Journals 27010.8.3 Web Sites 27110.9 Questions for Students 271

11 Astrobiology Experiments in Low Earth Orbit: Facilities,Instrumentation, and ResultsPietro Baglioni, Massimo Sabbatini, and Gerda Horneck

11.1 Low Earth Orbit Environment, a Test Bed for Astrobiology 27311.1.1 Cosmic Radiation Field in LEO 27511.1.1.1 Galactic Cosmic Radiation 27611.1.1.2 Solar Cosmic Radiation 27711.1.1.3 Radiation Belts 27811.1.2 Solar Extraterrestrial UV Radiation 27911.1.3 Space Vacuum 28011.1.4 Temperature Extremes 28011.1.5 Microgravity 28111.2 Astrobiology Questions Tackled by Experiments in Earth Orbit 28111.3 Exposure Facilities for Astrobiology Experiments 28211.3.1 BIOPAN 28311.3.1.1 Technical Characteristics of BIOPAN 28311.3.1.2 Experiment Hardware Accommodated within BIOPAN 28511.3.1.3 Operational Aspects of BIOPAN 28811.3.1.4 Orbital Characteristics of a BIOPAN Mission 29111.3.1.5 Environment of BIOPAN Experiments 29211.3.2 STONE 29311.3.3 EXPOSE 29511.3.3.1 EXPOSE Facility 29511.3.3.2 EXPOSE Experiments 29711.3.3.3 EXPOSE Experiment Hardware 29911.3.3.4 EXPOSE-R and EXPOSE-E 30111.3.3.5 Process of Experiment Proposal, Acceptance, Preparation,

and Validation 30211.4 Results from Astrobiology Experiments in Earth Orbit 30311.4.1 Relevance of Extraterrestrial Organic Molecules for the Emergence

of Life 30411.4.2 Role of Solar UV Radiation in Evolutionary Processes Related

to Life 30611.4.2.1 Efficiency of the Stratospheric Ozone Layer to Protect

Our Biosphere 30611.4.3 Chances and Limits of Life Being Transported from One Body of

Our Solar System to Another or Beyond 30711.4.3.1 Effects of Space Vacuum 309

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11.4.3.2 Effects of Extraterrestrial Solar UV Radiation 31011.4.3.3 Effects of Galactic Cosmic Radiation 31111.4.3.4 Combined Effects of All Parameters of Space 31311.4.3.5 Time Scales of Interplanetary Transport of Life 31311.4.4 Radiation Dosimetry in Space 31411.5 Future Development and Applications of Exposure Experiments 31611.6 Further Reading 31711.6.1 Books and Articles in Books 31711.6.2 Articles in Journals 31811.6.3 ESA Online Archives 31911.7 Questions for Students 319

12 Putting Together an Exobiology Mission: The ExoMars ExampleJorge L. Vago and Gerhard Kminek

12.1 Background of the ExoMars Mission 32112.1.1 Searching for Life on Mars 32112.1.2 Exobiology Research at ESA 32212.1.2.1 The ESA Exobiology Science Team Study 32412.1.2.2 The 1999 Exobiology Announcement of Opportunity 32512.1.3 The AURORA and the ELIPS Program of ESA 32612.1.3.1 The 2003 Pasteur Call for Ideas 32612.1.3.2 Approval of the ExoMars Mission 32812.2 ExoMars Science Objectives 32812.2.1 Searching for Signs of Life 32812.2.1.1 Extinct Life 32812.2.1.2 Extant Life 33212.2.1.3 Search for Life: Conclusions 33412.2.2 Hazards for Human Operations on Mars 33412.2.3 Geophysics Measurements 33512.3 ExoMars Science Strategy 33512.4 ExoMars Mission Description 33712.4.1 The ExoMars Rover 33912.5 Outlook and Conclusions 34512.6 Further Reading 34612.6.1 Books and Articles in Books 34612.6.2 Articles in Journals 34612.7 Questions for Students 351

13 Astrobiology Exploratory Missions and Planetary Protection RequirementsGerda Horneck, Andr� Debus, Peter Mani, and J. Andrew Spry

13.1 Rationale and History of Planetary Protection 35313.2 Current Planetary Protection Guidelines 35513.2.1 Category I Missions 35713.2.2 Category II Missions 35713.2.3 Category III Missions 359

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13.2.4 Category IV Missions 35913.2.5 Category V Missions 36013.2.6 Future Development of Planetary Protection Guidelines 36113.3 Implementation of Planetary Protection Guidelines 36213.3.1 Bioload Measurements 36313.3.2 Bioburden Reduction 36713.3.2.1 Surface Wiping with Biocleaning Agents 37113.3.2.2 Gamma Radiation Sterilization 37113.3.2.3 Dry-heat Sterilization 37213.3.2.4 Hydrogen Peroxide Vapor/Gas Plasma Sterilization 37213.3.3 Prevention of Recontamination 37313.4 Astrobiology Exploratory Missions of Concern to Planetary

Protection 37413.4.1 Missions to the Moon 37413.4.2 Missions to Mars 37613.4.2.1 Orbiters or Flyby Missions to Mars 37613.4.2.2 Landers or Rovers with in Situ Measurements 37813.4.2.3 Landers or Rovers with Martian Samples Returned to the Earth 38313.4.2.4 Human Missions to Mars 38713.4.3 Missions to Venus 38813.4.4 Missions to the Moons of the Giant Planets 38913.4.5 Missions to Asteroids or Comets 39013.5 Outlook: Future Tasks of Planetary Protection 39213.6 Further Reading 39413.6.1 Concerning COSPAR Planetary Protection Guidelines 39513.6.2 Concerning Handbooks and Standards on Planetary Protection 39513.6.3 Concerning Bioload of Spacecraft 39513.6.4 Concerning Lunar Missions 39613.6.5 Concerning Missions to Terrestrial Planets 39613.6.6 Concerning Missions to Jupiter’s Moon Europa 39713.7 Questions for students 397

Index 399

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Preface

Astrobiology is a relatively new research area that addresses questions that haveintrigued humans for a long time: “How did life originate?” “Are we alone in theUniverse?” “What is the future of life on Earth and in the Universe?” Thesequestions are jointly tackled by scientists converging from widely different fields,reaching from astrophysics to molecular biology and from planetology to ecology,among others.Whereas classical biological research has concentrated on the only example of

“life” so far known – life on Earth – astrobiology extends the boundaries ofbiological investigations beyond the Earth to other planets, comets, meteorites,and space at large. Focal points are the different steps of the evolutionary pathwaysthrough cosmic history that may be related to the origin, evolution, and distribu-tion of life. In the interstellar medium, as well as in comets and meteorites,complex organics are detected in huge reservoirs that eventually may provide thechemical ingredients for life. More and more data on the existence of planetarysystems in our Galaxy are being acquired that support the assumption thathabitable zones are frequent and are not restricted to our own Solar System.From the extraordinary ability of life to adapt to environmental extremes, theboundary conditions for the habitability of other bodies within our Solar Systemand beyond can be assessed. The final goal of astrobiology is to reveal the origin,evolution, and distribution of life on Earth and throughout the Universe in thecontext of cosmic evolution, and thereby to build the foundations for the con-struction and testing of meaningful axioms to support a theory of life.The multidisciplinary character of astrobiology is a challenge on the one hand

because it complies with modern science approaches; on the other hand, the fullexpertise in astrobiology is not always available at a single university. To overcomethis problem, experts from seven different European universities or researchcenters, specialized in leading fields of astrobiology, gathered in an astrobiologylecture course network with live tele-teaching and an interactive question-and-answer period. This book is based mainly on this multidisciplinary lecture series inastrobiology, and each chapter corresponds to a 90-minute lecture. The main fieldsof astrobiology are covered in a very competent and instructive manner.

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Complete Course in Astrobiology. Edited by Gerda Horneck and Petra RettbergCopyright � 2007 WILEY-VCH Verlag GmbH & Co. KGaA, WeinheimISBN: 978-3-527-40660-9

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The book starts with a general introduction to the fascinating world of astro-biology. The next chapters provide insights into the different steps of cosmicevolution, from the Big Bang through the formation of galaxies and stellar systems,with emphasis on the evolution of matter required for life: the elements andmolecules of life. The history of life on Earth is covered in the next chapters,including the latest results about the RNA world and concepts of a “window forlife“ as inferred from life’s strategies to adapt to factually every location on Earth.This leads to a definition of habitability that is applied to the planets and moons ofour Solar System, especially our neighbor planets Venus and Mars and thesatellites of the giant planets, Titan and Europa. With the advent of space explora-tion, space and the bodies of our Solar System are now within our reach; therefore,the technology required for astrobiology missions is also covered, exemplified byastrobiology experiments in low Earth orbit and astrobiology missions to Mars. Thebook concludes with a chapter on the legal and scientific issues of planetaryprotection required for each space mission within our Solar System.This book is intended as a textbook in astrobiology for students and teachers

from various fields of science that are interested in astrobiology. In each chapter, alist of questions for students is included. The CD is based on the original lecturesthat were given at the astrobiology lecture course network. The lectures can befollowed on the Web streaming network of the European Space Agency (ESA)(streamiss.spaceflight.esa.int) under “Astrobiology Lecture Course Network (a.y.2005–2006).”The editors and authors are grateful to the ESA for providing the platform and

support for realizing the Astrobiology Lecture Course Network that this book isbased on. Special thanks go to Daniel Sacotte, Director of Human Spaceflight,Microgravity and Exploration Programmes at ESA for providing continuous sup-port, and to Dieter Isakeit, Massimo Sabbatini, and their staff at the Erasmus UserCentre & Communication Office of ESA for their competent and efficient perform-ance in providing the required video production and infrastructure tools. Thanksgo to former and present coworkers and students of the authors for their contri-butions to the research in the different chapters. Special thanks go to the followingcolleagues or organizations: Frances Westall for collaboration on the postulate forhabitability, which Chapter 6 is based on, and for providing Figure 5.1; BirgitHuber for providing Figure 5.11; L�na Leroy for drawing Figure 3.2; Audrey Nobletfor drawing Figure 3.8; Rainer Facius for providing figures on cosmic radiation inChapter 11; and Gerhard Kminek for valuable comments on the ESA spacemissions and planetary protection for human missions in Chapter 13. Supportfor the laboratory work of Helga Stan Lotter (Chapter 5) by the Austrian FWFgrants P16260 and P18256 is gratefully acknowledged. The PPARC providedfinancial support for the research of Monica Grady (Chapter 8). We appreciatethe encouraging support from Christoph von Friedeburg and Nina Stadthaus fromthe Physics Department of Wiley-VCH, who gave us valuable advice during thepreparation of the book. During the editing process, we had continuous support byFolk Horneck, Lisa Steimel, and Thomas Urlings. Their commitment in reviewing

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and proofreading the manuscripts and in reworking electronic versions of thefigures is highly appreciated.

29 June 2006 Gerda HorneckPetra Rettberg

Cologne, Germany

Preface XVII

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1Astrobiology: From the Origin of Life on Earthto Life in the UniverseAndr� Brack

This chapter covers the different theories about the steps towardthe origin and evolution of life on Earth, and the major require-ments for these processes and for life at large are discussed.Conclusions are drawn on the likelihood of life originating andpersisting on other places of our Solar System, such as the ter-restrial planets and themoons of the giant planets, or beyond in theUniverse.

1.1General Aspects of Astrobiology

1.1.1Historical Milestones

Humans in every civilization have always been intrigued by their origin and theorigin of life itself. For thousands of years, the comforting theory of spontaneousgeneration seemed to provide an answer to this enduring question. In ancientChina, people thought that aphids were spontaneously generated from bamboos.Sacred documents from India mention the spontaneous formation of flies fromdirt and sweat. Babylonian inscriptions indicate that mud from canals was able togenerate worms.For the Greek philosophers, life was inherent to matter. It was eternal and

appeared spontaneously whenever the conditions were favorable. These ideaswere clearly stated by Thales, Democritus, Epicurus, Lucretius, and even by Plato.Aristotle gathered the different claims into a real theory. This theory safely crossedthe Middle Ages and the Renaissance. Famous thinkers such as Newton, Des-cartes, and Bacon supported the idea of spontaneous generation.The first experimental approach to the question was published in the middle of

the 17th century, when the Flemish physician Van Helmont reported the gener-

1.1 General Aspects of Astrobiology 1

Complete Course in Astrobiology. Edited by Gerda Horneck and Petra RettbergCopyright � 2007 WILEY-VCH Verlag GmbH & Co. KGaA, WeinheimISBN: 978-3-527-40660-9

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ation of mice from wheat grains and a sweat-stained shirt. He was quite amazed toobserve that they were identical to those obtained by procreation. A controversyarose in 1668, when Redi, a Toscan physician, published a set of experimentsdemonstrating that maggots did not appear when putrefying meat was protectedfrom flies by a thin muslin covering.Six years after Redi’s treatise, the Dutch scientist Anton Van Leeuwenhoek

observed microorganisms for the first time through a microscope that he madehimself. From then on, microorganisms were found everywhere and the support-ers of spontaneous generation took refuge in the microbial world. However, VanLeeuwenhoek was already convinced that the presence of microbes in his solutionswas the result of contamination by ambient air. In 1718, his disciple Louis Joblotdemonstrated that the microorganisms observed in solutions were, indeed,brought in from the ambient air, but he could not convince the naturalists.Even Buffon, in the middle of the 18th century, thought that nature was full of the

germs of life able to scatter during putrefaction and to gather again, later on, toreconstitute microbes. His Welsh friend John Needham undertook many experi-ments to support this view. He heated organic substances in water in a sealed flaskin order to sterilize the solutions. After a while, all solutions showed a profusion ofmicrobes. The Italian priest Lazzaro Spallanzani argued that the sterilization wasincomplete. He heated the solutions to a higher temperature and killed all themicrobes, but he could not kill the idea of microbial spontaneous generation.The controversy reached its apotheosis one century later when Felix Pouchet

published his treatise in 1860. He documented the theory of spontaneous gener-ation in the light of experiments that, in fact, were the results of contamination byambient air. Pasteur gave the finishing blow to spontaneous generation in June1864 when he designed a rigorous experimental set up for sterilization. By usingflasks with long necks that had several bends and were filled with sterilized brothor urine, he showed that no life appeared in the infusions as long as the flaskremained intact.The beautiful demonstration of Pasteur opened the fascinating question of the

historical origin of life. Because life can originate only from preexisting life, it has ahistory and therefore an origin, which must be understood and explained bychemists.Charles Darwin first formulated the modern approach to the chemical origin of

life. In February 1871, he wrote in a private letter to Hooker:

If (and oh, what a big if) we could conceive in some warm littlepond, with all sorts of ammonia and phosphoric salts, light, heat,electricity, etc., present that a protein compound was chemicallyformed, ready to undergo still more complex changes, at the presentday such matter would be instantly devoured or adsorbed, whichwould not have been the case before living creatures were formed.

For 50 years, the idea lay dormant. In 1924, the young Russian biochemistAleksander Oparin pointed out that life must have arisen in the process of theevolution of matter thanks to the nature of the atmosphere, which was considered

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to be reducing. In 1928, the British biologist J. B. S. Haldane, independently ofOparin, speculated on the early conditions suitable for the emergence of life.Subjecting a mixture of water, carbon dioxide, and ammonia to UV light shouldproduce a variety of organic substances, including sugars and some of the materi-als from which proteins are built up. Before the emergence of life they must haveaccumulated in water to form a hot, dilute “primordial soup.” Almost 20 years afterHaldane’s publication, J. D. Bernal conjectured that clay mineral surfaces wereinvolved in the origin of life. In 1953, Stanley Miller, a young student of HaroldUrey, reported the formation of four amino acids – glycine, alanine, aspartic acidand glutamic acid – when he subjected a mixture of methane, ammonia, hydrogen,and water to electric discharges. Miller’s publication really opened the field ofexperimental prebiotic chemistry (see Chapter 3).

1.1.2Searching for Emerging Life

Defining life is a difficult task, and the intriguing and long lasting question “Whatis life?” has not yet received a commonly accepted answer, even for what could bedefined as minimal life, the simplest possible form of life. On the occasion of aWorkshop on Life, held in Modena, Italy, in 2003, each member of the Interna-tional Society for the Study of the Origins of Life was asked to give a definition oflife. The 78 different answers occupy 40 pages in the proceedings of the workshop.Perhaps the most general working definition is that adopted in October 1992 by

the NASA Exobiology Program: “Life is a self-sustained chemical system capable ofundergoing Darwinian evolution.” Implicit in this definition is the fact that thesystem uses external matter and energy provided by the environment. In otherwords, primitive life can be defined, a minima, as an open chemical system capableof self-reproduction, i.e., making more of itself by itself, and capable of evolving.The concept of evolution implies that the chemical system normally transfers itsinformation fairly faithfully but makes a few random errors. These may potentiallylead to higher complexity/efficiency and possibly to better adaptation to changes inthe existing environmental constraints.Schematically, the premises of an emerging life can be compared to parts of

“chemical robots.” By chance, some parts self-assembled to generate robots capableof assembling other parts to form identical robots. Sometimes, a minor error in thebuilding generated more efficient robots, which became the dominant species.In a first approach, present life, based on carbon chemistry in water, is generally

used as a reference to provide guidelines for the study of the origins of life and forthe search for extraterrestrial life. It is generally assumed that the primitive robotsemerged in liquid water and that the parts were already organic molecules. Theearly molecules that contain carbon and hydrogen atoms associated with oxygen,nitrogen, and sulfur atoms are often called the CHONS, where C stands for carbon,H for hydrogen, O for oxygen, N for nitrogen, and S for sulfur.

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1.1.3The Role of Water

Liquid water played a major role in the appearance and evolution of life by favoringthe diffusion and exchange of organic molecules. Liquid water has many pecu-liarities. Water molecules establish hydrogen bonds with molecules containinghydrophilic groups. In water, organic molecules containing both hydrophilic andhydrophobic groups self-organize in response to these properties. This dualitygenerates interesting prebiotic situations, such as the stereo-selective aggregationof short peptide sequences of alternating hydrophobic– hydrophilic residues intothermostable �-sheet structures endowed with chemical activity, as shown below.In addition to H-bonding capability, water exhibits a large dipole moment

(1.85 debye) as compared to alcohols (<1.70 debye). This large dipole momentfavors the dissociation of ionizable groups such as -NH2- and -COOH-generatingionic groups, which can form additional H bonds with water molecules, thusimproving their solubility.With a high dielectric constant � of 80, water is an outstanding dielectric

compound. When organic groups with opposite charges Q and Q 0, separated bya distance r, are formed, their recombination is unfavorable because the force ofattraction for reassociation is given by

F ¼ Q �Q 0=�� r2. (1.1).

This is also true for metal ions, which have probably been associated with organicmolecules since the beginning of life.Liquid water was probably active in prebiotic chemistry as a clay producer and

heat dissipator. Further, liquid water is a powerful hydrolytic chemical agent. Assuch, it allows pathways for chemical combinations that would have few chances tooccur in an organic solvent. Liquid water is therefore generally considered as aprerequisite for the emergence of life on Earth.

1.1.4The Physicochemical Features of Carbon-based Life

Life is autocatalytic in essence and is able to evolve. To evolve, i.e., to increase itsdiversity, the molecules bearing the hereditary memory must be able to be ex-tended and diversified by combinatorial dispersive reactions. This can best beachieved with a scaffolding of polyvalent atoms. From a chemical viewpoint, carbonchemistry is by far the most productive in this respect. Another clue in favor ofcarbon is provided by radio astronomers: about 90 carbon-containing moleculeshave been identified in the interstellar medium while only 9 silicon-based mole-cules have been detected (see Chapter 2). To generalize, a carbon-based life is notjust an anthropocentric view, it appears as a highly plausible prerequisite.Carbon atoms exhibit two remarkable features relative to life, one-handedness

and stable isotope distribution. One-handedness, also called homochirality (from

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the Greek kheiros, the hand), of the proteins synthesized via the genetic code is acharacteristic of all living systems (see Chapter 3). Each central carbon atom of theamino acid molecule occupies the center of a tetrahedron. Except for the aminoacid glycine, the four substituents of the central carbon atom are different. Thecarbon atom is therefore asymmetrical and it is not superimposable onto its mirrorimage. Each amino acid exists in twomirror-image forms called enantiomers (fromthe Greek enantios, opposed). All protein amino acids have the same handedness:they are homochiral. They are left-handed and hence known as L-amino acids.Their right-handed mirror images are known as D-amino acids. L-amino acidsengaged in a protein chain generate right-handed, single-strand Æ-helices andasymmetrical, multi-strand �-sheet structures. Nucleotides, the building blocksof the nucleic acids DNA and RNA, are also homochiral. Their nomenclature ismore complex because each nucleotide possesses four asymmetrical carbon atoms.In this case, the geometry of a selected carbon atom was chosen. Following thisconvention, nucleotides are right-handed. Right-handed nucleotides generallygenerate right-handed helical nucleic acids.Pasteur was probably the first to realize that biological asymmetry could best

distinguish between inanimate matter and life. Life that would simultaneously useboth right- and left-handed forms of the same biological molecules appears veryunlikely for geometrical reasons. For example, enzyme �-pleated sheets cannotform when both L- and D-amino acids are present in the same molecule. Becausethe catalytic activity of an enzyme is intimately dependent upon the geometry of thechain, the absence of �-pleated sheets would impede, or at least considerablyreduce, the activity spectrum of the enzymes. The use of one-handed biomonomersalso sharpens the sequence information of the biopolymers. For a polymer made ofn units, the number of sequence combinations will be divided by 2 n when thesystem uses only homochiral (one-handed) monomers. Taking into account thefact that enzyme chains are generally made up of hundreds of monomers, and thatnucleic acids contain several million nucleotides, the tremendous gain in simplic-ity offered by the use of monomers restricted to one handedness is self-evident.Finally, if the biopolymers to be replicated were to contain L- and D-units located

at specific sites, the replication process would have to not only be able to positionthe right monomers at the right place but also select the right enantiomer fromamong two species, which differ only by the geometry of the asymmetrical carbonatoms. For example, the bacterium Bacillus brevis is able to synthesize the peptidegramicidin A, which is constructed on a strict alternation of left- and right-handedamino acids. However, the biosynthesis of this peptide involves a set of complexand sophisticated enzymes that are homochiral.Life on Earth uses homochiral left-handed amino acids and right-handed sugars.

A mirror-image life, using right-handed amino acids and left-handed sugars, isperfectly conceivable and might have developed on another planet. Thus, homo-chirality is generally considered a crucial signature for life.The uptake of carbon dioxide by living systems can produce biomolecules

enriched in 12C carbon isotopes at the expense of 13C isotopes. For example, onEarth, over 1600 samples of fossil kerogen (a complex organic macromolecule

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produced from the debris of biological matter) have been compared with carbo-nates in the same sedimentary rocks. The organic matter is enriched in 12C byabout 25‰. This offset is now taken to be one of the most powerful indications thatlife on Earth was active nearly 3.9 billion years ago, because the sample suiteencompasses specimens right across the geologic timescale.

1.1.5Clays as Possible Primitive Robots

Any scientist who has observed the crystallization of minerals initiated by theaddition of seeds to a supersaturated solution is tempted to associate life withmineral crystals. Jean Schneider, for example, suggested that complex dislocationnetworks encountered in crystals may, in some cases, follow the criteria of livingunits and lead to a crystalline physiology. He also discussed the places of possibleoccurrence in nature of this kind of physiology, such as terrestrial and extraterres-trial rocks, interplanetary dust, white dwarfs, and neutron stars.According to Cairns-Smith, there is no compelling reason to necessarily relate

the last common ancestor made of organic molecules with first life. Although theeasy accessibility of numerous organic building blocks of life has been demon-strated experimentally, the dominant use of these molecules in living organismscan be seen as a result of evolution rather than a prerequisite for its initiation.Cairns-Smith proposed that the first living systems, and the chemical evolutionpreceding it, might have been based on a chemistry different from that which weknow. The structurally and functionally complex genetic system of modern lifearose subsequently in a living organism using a less efficient primary system witha much higher probability of spontaneous assembly. As genetic candidates, headvocated crystalline inorganic materials presenting suitable properties, such asthe ability to store and replicate information in the form of defaults, dislocations,and substitutions. Clay minerals, such as kaolinite, are particularly attractivebecause they form at ambient temperatures from aqueous weathering of silicaterock.The following “genetic takeover” scenario was proposed by Cairns-Smith as a

mineral origin of life. Certain clays having properties that favor their synthesisproliferated, and their replication defects, likewise, became more common. Incertain clay lineages, the development of crude photochemical machinery favoredthe synthesis of some non-clay species, such as polyphosphates and small organiccompounds. Natural selection favored these lineages of clays because the organiccompounds they produce catalyzed the clay formation. Multiple-step pathways ofhigh specificity, including chiral stereoselection, arose through specific adsorption,followed by the appearance of polymers of specified sequence, at first serving onlystructural roles. Base-paired polynucleotides replicated, giving rise to secondaryand minor genetic material. This secondary material proved to be useful in thealignment of amino acids for polymerization. The ability to produce specificenzymes came concomitantly with the ability to produce sequence-specified poly-peptides and proteins. More-efficient pathways of organic synthesis ensued, and

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finally the clay machinery was dispensed with in favor of a polynucleotide-basedreplication–translation system. Although each step of the hypothetical sequence ofevents was developed in detail, the scenario has not been supported by experimen-tal facts.

1.2Reconstructing Life in a Test Tube

It is now a generally accepted conception that life emerged in water and that thefirst self-reproducing molecules and their precursors were probably organic mol-ecules built up with carbon atom skeletons. Organic molecules were formed fromgaseous molecules containing carbon atoms (methane, carbon dioxide, carbonmonoxide), nitrogen atoms (nitrogen, ammonia), or sulfur atoms (hydrogen sul-fide, sulfur oxide). The energy for these reactions came from electric discharges,cosmic and UV radiation, or heat.

1.2.1The Quest for Organic Molecules

1.2.1.1 Terrestrial ProductionIn 1953, Stanley Miller exposed a mixture of methane, ammonia, hydrogen, andwater to electric discharges to mimic the effects of lightning. Among the com-pounds formed, he identified 4 of the 20 naturally occurring amino acids, thebuilding blocks of proteins. Since this historic experiment, 17 natural amino acidshave been obtained via the intermediate formation of simple precursors, such ashydrogen cyanide and formaldehyde. It has been shown that spark dischargesynthesis of amino acids occurs efficiently when a reducing gas mixture containingsignificant amounts of hydrogen is used (see Chapter 3). However, the truecomposition of the primitive Earth atmosphere remains unknown. Today, geo-chemists favor a non-reducing atmosphere dominated by carbon dioxide. Undersuch conditions, the production of amino acids appears to be very limited. Stronglyreducing environments capable of reducing carbon dioxide were necessary for thesynthesis of amino acids.Deep-sea hydrothermal systems may represent suitable reducing environments

for the synthesis of prebiotic organic molecules. The ejected gases contain carbondioxide, carbon monoxide, sulfur dioxide, nitrogen, and hydrogen sulfide. Forinstance, high concentrations of hydrogen (more than 40% of the total gas) andmethane have been detected in the fluids of the Rainbow ultramafic hydrothermalsystem of the Mid-Atlantic Ridge. The production of hydrogen, a highly reducingagent favoring prebiotic syntheses, is associated with the hydrous alteration ofolivine into serpentine and magnetite, a reaction known as “serpentinization.”Indeed, hydrocarbons containing 16 to 29 carbon atoms have been detected inthese hydrothermal fluids. Amino acids have been obtained, although in low yields,under conditions simulating these hydrothermal vents.

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According to W�chtersh�user (1994), primordial organic molecules formed nearthe hydrothermal systems; the energy source required to reduce the carbon dioxidemight have been provided by the oxidative formation of pyrite (FeS2), from ironsulfide (FeS) and hydrogen sulfide (H2S). Pyrite has positive surface charges andbonds the products of carbon dioxide reduction, giving rise to a two-dimensionalreaction system, a “surface metabolism.” Laboratory work has provided support forthis promising new “metabolism-first” approach. Iron sulfide, hydrogen sulfide,and carbon dioxide react under anaerobic conditions to produce hydrogen and aseries of thiols, including methanethiol. Methanethiol and acetic acid have alsobeen obtained from carbon monoxide, hydrogen sulfide, iron and nickel sulfides,and catalytic amounts of selenium. Under specific conditions, thioesters areformed that might have been the metabolic driving force of a “thioester world,”according to de Duve (1998). Thioesters are sulfur-bearing organic compounds thatpresumably would have been present in a sulfur-rich, volcanic environment on theearly Earth.Hydrothermal vents are often disqualified as efficient reactors for the synthesis

of bioorganic molecules because of their high temperature. However, the productsthat are synthesized in hot vents are rapidly quenched in the surrounding coldwater, which may preserve those organics formed.

1.2.1.2 Delivery of Extraterrestrial Organic MoleculesComets and meteorites may have delivered important amounts of organic mole-cules to the primitive Earth (see Chapter 3). Nucleic acid bases, purines, andpyrimidines have been found in the Murchison meteorite. One sugar (dihydroxy-acetone), sugar alcohols (erythritol, ribitol), and sugar acids (ribonic acid, gluconicacid) have been detected in the Murchison meteorite, but ribose, the sugar moietyof ribonucleotides, themselves the building blocks of RNAs (see Chapter 4), has notbeen detected.Eight proteinaceous amino acids have been identified in one such meteorite,

amongmore than 70 amino acids found therein. Cronin and Pizzarello (1997) foundan excess of about 9% of L-enantiomers for some non-protein amino acids detectedin the Murchison meteorite. The presence of L-enantiomeric excesses in thesemeteorites points towards an extraterrestrial process of asymmetric synthesis ofamino acids asymmetry that is preserved inside the meteorite. These excesses mayhelp us to understand the emergence of biological asymmetry or one-handedness.The excess of one-handed amino acids found in the meteorites may result from theprocessing of the organicmantles of the interstellar grains fromwhich themeteoritewas originally formed. That processing could occur, for example, by the effects ofcircularly polarized synchrotron radiation from a neutron star, a remnant of asupernova. On the other hand, strong infrared circular polarization, resultingfromdust scattering in reflection nebulae in theOrionOMC-1 star formation region,has been observed by Bailey. Circular polarization at shorter wavelengthsmight havebeen important in inducing this chiral asymmetry in interstellar organic moleculesthat could be subsequently delivered to the early Earth.

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Dust collection in the Greenland and Antarctic ice sheets and its analysis byMaurette show that the Earth captures interplanetary dust as micrometeorites at arate of about 20 000 tons per year. About 99% of this mass is carried by micro-meteorites in the 50–500 �m size range. This value is much higher than the mostreliable estimate of the normal meteorite flux, which is about 10 tons per year. Ahigh percentage of micrometeorites in the 50–100 �m size range have been ob-served to be unmelted, indicating that a significant fraction traversed the terrestrialatmosphere without drastic heating. In this size range, the carbonaceous micro-meteorites represent 20% of the incoming micrometeorites, and they contain 2.5%carbon on average. This flux of incoming micrometeorites might have brought tothe Earth about 2.5 � 1022 g carbon over the period corresponding to the late heavybombardment. As inferred from the lunar craters, during this period planetesimals,asteroids, and comets impacted the Earth until about 3.85 billion years ago (seeChapter 2). For comparison, this delivery represents more carbon than is in thepresent surficial biomass, which amounts to about 1018 g. In addition to organiccompounds, these grains contain a high proportion of metallic sulfides, oxides, andclay minerals that belong to various classes of catalysts. In addition to the carbona-ceous matter, micrometeorites might also have delivered a rich variety of catalysts.These may have functioned as tiny chemical reactors when reaching oceanic water.On 15 January 2006, the Stardust reentry probe brought cometary grains to the

Earth for the first time. The preliminary analyses of these grains from comet Wild-2 confirmed that micrometeorites are probably witnesses of a chemical continuum– via the cometary grains – from the interstellar medium, where they form, toterrestrial oceans. Comets are the richest planetary objects in organic compoundsknown so far. Ground-based observations have detected hydrogen cyanide andformaldehyde in the coma of comets.In 1986, onboard analyses performed by the two Russian missions Vega 1 and

Vega 2, as well as observations obtained by the European mission Giotto and thetwo Japanese missions Suisei and Sakigake, demonstrated that Halley’s Cometshows substantial amounts of organic material. On average, dust particles ejectedfrom Halley’s nucleus contain 14% organic carbon by mass. About 30% ofcometary grains were dominated by the light elements C, H, O, and N, and 35%are close in composition to the carbon-rich meteorites. The presence of organicmolecules, such as purines, pyrimidines, and formaldehyde polymers, has beeninferred from the fragments analyzed by the Giotto PICCA and Vega PUMA massspectrometers. However, there was no direct identification of the complex organicmolecules probably present in the cosmic dust grains and in the cometary nucleus.Many chemical species of interest for exobiology were detected in Comet Hya-

kutake in 1996, including ammonia, methane, acetylene (ethyne), acetonitrile(methyl cyanide), and hydrogen isocyanide. The study of the Hale-Bopp Cometin 1997 led to the detection of methane, acetylene, formic acid, acetonitrile, hydro-gen isocyanide, isocyanic acid, cyanoacetylene, formamide, and thioformaldehyde.It is possible, therefore, that cometary grains might have been an important

source of organic molecules delivered to the primitive Earth. Comets orbit onunstable trajectories and sometimes collide with planets. The collision of Comet

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Shoemaker-Levy 9 with Jupiter in July 1994 is a recent example of such an event.Such collisions were probably more frequent 4 billion years ago, when the cometsorbiting around the Sun were more numerous than today. By impacting the Earth,comets probably delivered a substantial fraction of the terrestrial water (about 35%according to the estimation of Owen based on the relative contents in hydrogen anddeuterium) in addition to organic molecules. The chemistry that is active at thesurface of a comet is still poorly understood. The European mission Rosetta,launched in 2004, will analyze the nucleus of the comet 67 P/Churyumov-Ger-asimenko. The spacecraft will first study the environment of the comet during aflyby over several months, and then a probe will land to analyze the surface and thesubsurface ice sampled by drilling.

1.2.2Space Experiments

Ultraviolet (UV) irradiation of dust grains in the interstellar medium may result inthe formation of complex organic molecules. The interstellar dust particles areassumed to be composed of silicate grains surrounded by ices of different mole-cules, including carbon-containing molecules (see Chapter 3). In a laboratoryexperiment, ices of H2O, CO2, CO, CH3OH, and NH3 were deposited at 12 K undera pressure of 10–5 Pa (10–7 mbar) and were then irradiated by electromagneticradiation representative of that in the interstellar medium. The solid layer thatdeveloped on the solid surface was analyzed by enantioselective gas chromatog-raphy coupled with mass spectrometry (GC-MS). After the analytical steps ofextraction, hydrolysis, and derivatization, 16 amino acids were identified in thesimulated ice mantle of interstellar dust particles. These experiments confirmedthe preliminary amino acid formation obtained first by Greenberg. The chiralamino acids were identified as being totally racemic (consisting of equal amountsof D- and L-enantiomers). Parallel experiments performed with 13C-containingsubstitutes definitely excluded contamination by biological amino acids. Theresults strongly suggest that amino acids are readily formed in interstellar space.Before reaching the Earth, organic molecules are exposed to UV radiation, both

in interstellar space and in the Solar System. Amino acids have been exposed inEarth orbit to study their survival in space. The UV flux of wavelengths <206 nm inthe diffuse interstellar medium is about 108 photons cm–2 s–1. In Earth orbit, thecorresponding solar flux is in the range of 1016 photons cm–2 s–1. This means thatan irradiation over one week in Earth orbit corresponds to that over 275 000 years inthe interstellar medium. Thin films of amino acids, like those detected in theMurchison meteorite, have been exposed to space conditions in Earth orbit withinthe BIOPAN facility of the European Space Agency (ESA) onboard the unmannedRussian satellites Foton 8 and Foton 11 (see Chapter 11). Aspartic acid and glutamicacid were partially destroyed during exposure to solar UV. However, decomposi-tion was prevented when the amino acids were embedded in clays.Amino acids and peptides have also been subjected to solar radiation outside the

MIR station for 97 days. After three months of exposure, about 50% of the amino

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acids were destroyed in the absence of mineral shielding. Peptides exhibited anoticeable sensitivity to space vacuum, and sublimation effects were detected.Decarboxylation was found to be the main effect of photolysis. No polymerizationoccurred and no racemization (the conversion of L- or D-amino acids into a racemicmixture) was observed. Some samples were embedded into mineral material(montmorillonite clay, basalt, or Allendemeteorite) when exposed to space. Amongthe different minerals, the meteoritic powder offered the best protection, whereasthe clay montmorillonite was the least efficient. Different thicknesses of meteoritepowder films were used to estimate the shielding threshold. Significant protectionfrom solar UV radiation was observed when the thickness of the meteorite mineralwas 5 �m or greater.

1.2.3Attempts to Recreate Life in a Test Tube

By analogy with contemporary living systems, it was long considered that primitivelife emerged as cellular entities, requiring boundary molecules able to isolate thesystem from the aqueous environment (membrane). Further, catalytic moleculeswould be needed to provide the basic chemical work of the cell (enzymes), as well asinformation-retaining molecules that allow the storage and transfer of the infor-mation needed for replication (RNA).Fatty acids are known to form vesicles when the hydrocarbon chains containmore

than 10 carbon atoms. Such vesicle-forming fatty acids have been identified in theMurchison meteorite by Deamer (1985). However, the membranes obtained withthese simple amphiphiles are not stable over a broad range of conditions. Stableneutral lipids can be obtained by condensing fatty acids with glycerol or with glycerolphosphate, thus mimicking the stable contemporary phospholipid. Primitive mem-branes also could initially have been formed by simple isoprene derivatives.Most of the catalytic chemical reactions in a living cell are achieved by proteina-

ceous enzymes made of 20 different homochiral L-amino acids. Amino acids weremost likely available on the primitive Earth as complex mixtures, but the formationof mini-proteins from the monomers in water is not energetically favored. Becausethe peptide bond of proteins is thermodynamically unstable in water, it requires anenergy source, such as heat or condensing chemicals, to link two amino acidstogether in an aqueous milieu. Oligoglycines up to the octamer have been obtainedfrom glycine in a flow reactor simulating hydrothermal circulation. These com-pounds were formed by repeatedly circulating solutions of glycine and CuCl2 froma high-pressure, high-temperature chamber to a high-pressure, low-temperaturechamber, simulating conditions in a hydrothermal vent. Clays and salts may alsobe used to condense free amino acids in water. When subjecting mixtures ofglycine and kaolinite to wet–dry cycles and 25–94 �C temperature fluctuations,the formation of oligopeptides up to five glycines long has been observed.Bulk thermal condensation of amino acids has been described by Fox, who has

shown that dry mixtures of amino acids polymerize when heated to 130�C to give“proteinoids.” In the presence of polyphosphates, the temperature can be decreased

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to 60�C. High molecular weights were obtained when an excess of acidic or basicamino acids was present. In aqueous solutions, the proteinoids aggregated sponta-neously to form microspheres of 1–2 �m, presenting an interface resembling thelipid bilayers of living cells. The microspheres increased slowly in size from dis-solved proteinoids and were sometimes able to bud and to divide. These micro-spheres were described as catalyzing the decomposition of glucose and were able towork as esterases and peroxidases. The main advantage of proteinoids is theirorganization into particles, but they also represent a dramatic increase in complexity.The number of condensing agents capable of assembling amino acids into

peptides in water is limited, especially when looking for prebiotically plausiblecompounds. Carbodiimides, having a general formula R-N=C=N-R', power theligation of both glutamic and aspartic acids on hydroxyapatite. The simplestcarbodiimide, H-N=C=N-H, can be considered a transposed form of cyanamide(NH2-CN), which is present in the interstellar medium. In water, cyanamide formsa dimer, dicyandiamide, which is as active as carbodiimides in forming peptides.However, the reactions are very slow and do not proceed beyond the tetrapeptide.Oligomers of glutamic acid greater than 45 amino acids in length were formed

on hydroxyapatite and illite after 50 feedings with glutamic acid and the condens-ing agent carbonyldiimidazole (Im-CO-Im). Amino acid adenylate anhydrides havebeen reported to condense readily in the presence of montmorillonite. According tode Duve (1998), the first peptides may have appeared via thioesters, which generateshort peptides in the presence of mineral surfaces. Among the most effectiveactivated amino acid derivatives for the formation of oligopeptides in aqueoussolution are the N-carboxyanhydrides.Chemical reactions capable of selectively condensing protein amino acids more

readily than non-protein ones have been described. Helical and sheet structuresmay be modeled with the aid of only two different amino acids, the first one beinghydrophobic and the second hydrophilic. Polypeptides with alternating hydro-phobic and hydrophilic residues adopt a water-soluble �-sheet geometry becauseof hydrophobic side-chain clustering. Because of the formation of �-sheets, alter-nating sequences display a good resistance toward chemical degradation. Aggre-gation of alternating sequences into �-sheets is possible only with homochiral (allL or all D) polypeptides, as demonstrated by this author at the Centre de Bio-physique Mol�culaire in Orl�ans, France. Short peptides have also been found toexhibit catalytic properties.In contemporary living systems, the hereditary memory is stored in nucleic acids

built up with bases (purine and pyrimidine), sugars (ribose for RNA, deoxyribosefor DNA), and phosphate groups. The accumulation of significant quantities ofnatural RNA nucleotides does not appear to be a plausible chemical event on theprimitive Earth. Purines are easily obtained from hydrogen cyanide or by subject-ing reduced gas mixtures to electric discharges. No successful pyrimidine synthesisfrom electrical discharges has been published so far, whereas hydrogen cyanideaffords only very small amounts of these bases. Condensation of formaldehydeleads to ribose as well as a large number of other sugars. Although the synthesis ofpurine nucleosides (the combination of purine and ribose) and of nucleotides has

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been achieved by heating the components in the solid state, the yields are very lowand the reactions are not regioselective. Interestingly, very effective montmorillon-ite-catalyzed condensation of nucleotides into oligomers up to 55 monomers longhas been reported by Ferris from nucleoside phosphorimidazolides.The synthesis of oligonucleotides is much more efficient in the presence of a

preformed, pyrimidine-rich polynucleotide acting as a template. Non-enzymaticreplication has been demonstrated by Orgel. The preformed chains align thenucleotides by base-pairing to form helical structures that bring the reactinggroups into close proximity. However, the prebiotic synthesis of the first oligonu-cleotide chains remains an unsolved challenge.

1.2.4A Primitive Life Simpler than a Cell?

Thomas Cech found that some RNAs, the ribozymes, have catalytic properties (seeChapter 4). For example, they increase the rate of hydrolysis of oligoribonucleotides.They also act as polymerization templates, because chains up to 30 monomers longcan be obtained starting from a pentanucleotide. Since this primary discovery, thecatalytic spectrumof these ribozymes has been considerably enlarged by the directedtest tube molecular evolution experiments initiated in the laboratories of GeraldJoyce and Jack Szostak. Since RNA was shown to be able to act simultaneously asgeneticmaterial and as a catalyst, RNAhas been considered the first living systemonthe primitive Earth (the “RNA world”). This is because it can simultaneously be thegenotype and the phenotype and can fulfill the basic cycle of life consisting of self-replication, mutation, and selection. Strong evidence for this proposal has beenobtained from the discovery that modern protein synthesis in the ribosome iscatalyzed by RNA. One should, however, remember that RNAs synthesis underprebiotic conditions remains an unsolved challenge. It seems unlikely that lifestarted with RNA molecules, because these molecules are not simple enough. TheRNA world appears to have been an episode in the evolution of life before theappearance of cellular microbes rather than the spontaneous birth of life.RNA analogues and surrogates have been studied. The initial proposal was that

the first RNA was a flexible, achiral derivative in which ribose was replaced byglycerol, but these derivatives did not polymerize under prebiotic conditions. Theease of forming pyrophosphate (double phosphate) bonds prompted investigationof linking nucleotides by pyrophosphate groups. This proposal was tested using thereactions of the diphosphorimidazolides of deoxynucleotides. Their reaction in thepresence of magnesium or manganese ions resulted in the formation of 10–20mers of the oligomers.Considering the ease of formation of hexose-2,4,6-triphosphates from glycolal-

dehyde phosphate in a process analogous to the formose reaction, Eschenmoserand coworkers chemically synthesized polynucleotides containing hexopyranoseribose (pyranosyl-RNA or p-RNA) in place of the usual “natural” pentofuranoseribose found in RNA. p-RNAs form Watson-Crick-paired double helices that aremore stable than RNA. Furthermore, the helices have only a weak twist, which

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should make it easier to separate strands during replication. Replication experi-ments have had marked success in terms of sequence copying but have failed todemonstrate template-catalysis turnover numbers greater than 1. The chemicalsynthesis of threo furanosyl nucleic acid (TNA), an RNA analogue built on thefuranosyl form of the tetrose sugar threose, was also reported by the Eschenmosergroup. TNA strands are much more stable in aqueous solution than RNA and areresistant to hydrolysis. They form complementary duplexes between complemen-tary strands. Moreover, of even greater potential importance, they form comple-mentary strands with RNA. This raises the possibility that TNAs could have servedas templates for the formation of complementary RNAs by template-directedsynthesis. TNA is a more promising precursor to RNA than p-RNA, becausetetroses have the potential to be synthesized from glycolaldehyde phosphate andtwo other carbon precursors, which may have been present in quantities greaterthan those of ribose on the primitive Earth.Peptide nucleic acids (PNA), first synthesized by Nielsen and coworkers, consist

of a peptide-like backbone to which nucleic acid bases are attached. PNAs form verystable double-helical structures with complementary strands of PNA (PNA-PNA),DNA (PNA-DNA), RNA (PNA-RNA), and even stable PNA2-DNA triple helices.Information can be transferred from PNA to RNA, and vice versa, in template-directed reactions. Although PNA hydrolyzes rather rapidly, thus considerablyrestricting the chances of PNA ever having accumulated in the primitive terrestrialoceans, the PNA-PNA double helix illustrates that genetic information can bestored in a broad range of double-helical structures.Chemists are also tempted to consider that primitive self-replicating systems

must have used simpler informational molecules than biological nucleic acids ortheir analogues. Because self-replication is, by definition, autocatalysis, they aresearching for simple autocatalytic molecules capable of mutation and selection.Reza Ghadiri tested peptides as possible templates, and non-biological organicmolecules have been screened by G�nter von Kiedrowski. In most cases, the rate ofthe autocatalytic growth was not linear. The initial rate of autocatalytic synthesiswas found to be proportional to the square root of the template concentration: thereaction order in these autocatalytic self-replicating systems was found to be 1/2rather than 1, a limiting factor as compared to most autocatalytic reactions knownso far. Autocatalytic reactions are particularly attractive because they might amplifysmall enantiomeric excesses, eventually extraterrestrial, to homochirality.

1.3The Search for Traces of Primitive Life

1.3.1Microfossils

The first descriptions of fossil microorganisms in the oldest, well-preserved sedi-ments (3.5–3.3 billion years old) from Australia and South Africa were made by

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William Schopf and Elso Barghoorn. Although their observations have been calledinto question, Westall and others have more recently established that life wasabundant in these rocks. From a theoretical point of view, the earliest forms of lifewould most likely have had a chemolithoautotrophic metabolism, using inorganicmaterials as a source of both carbon and energy. Evidence for the presence ofchemolithotrophs in the hydrothermal deposits from Barberton and the Pilbaracomes from the N and C isotopic data. Considering the high temperatures on theearly Earth, it is probable that the earliest microorganisms were thermophilic.Structures resembling oxygenic photosynthetic microorganisms such as cyanobac-teria have been described, and carbon isotope data have been interpreted asevidence for their presence. However, these interpretations are strongly disputed.Nevertheless, the fact that the microorganisms inhabiting the early Archeanenvironments of Barberton (South Africa) and Pilbara (Australia) formed matsin the photic zone suggests that some of them may already have developedanoxygenic photosynthesis.

1.3.2Oldest Sedimentary Rocks

The oldest sedimentary rocks occur in southwest Greenland and have been dated at3.8–3.85 billion years by Manfred Schidlowski and Stephen Mozsis. The old sedi-ments testify to the presence of permanent liquid water on the surface of the Earthand to the presence of carbon dioxide in the atmosphere. They contain organiccarbon. Minik Rosing found that the isotopic signatures of the organic carbonfound in Greenland meta-sediments provide indirect evidence that life may be 3.85billion years old. Taking the age of the Earth as about 4.6 billion years, this meansthat life must have begun quite early in Earth’s history. Although there are seriousreservations concerning these studies (contamination by more recent fossilizedendoliths, 12C enrichment produced by thermal decomposition of siderite andmetamorphic processes), stepped combustion analysis by Mark von Zuilen hasverified the existence of the 12C enrichment in these sediments.

1.4The Search for Life in the Solar System

1.4.1Planet Mars and the SNC Meteorites

The mapping of Mars by the spacecrafts Mariner 9, Viking 1 and Viking 2, MarsGlobal Surveyor, and Mars Express revealed channels and canyons resembling dryriverbeds (see Chapter 8). The gamma-ray spectrometer instrument onboard theMars orbiter Odyssey detected hydrogen, which indicates the presence of water icein the upper meter of soil in a large region surrounding the planet’s south pole,where ice is expected to be stable. The amount of hydrogen detected indicates 20–

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50% ice by mass in the lower layer beneath the topmost surface. The ice-rich layeris about 60 cm beneath the surface at latitude 60 ºS and approaches 30 cm of thesurface at latitude 75 ºS. The ancient presence of liquid water on the surface ofMars was confirmed by the two AmericanMars Exploration Rovers (MER A and B),Spirit and Opportunity, and by the presence of sulfates and clays revealed by theinfrared spectrometer OMEGA onboard the European Mars orbiter Mars Express.However, Martian oceans were probably restricted to the very early stages ofMartian history. Mars therefore possessed an atmosphere capable of deceleratingcarbonaceous micrometeorites, and chemical evolution may have been possible onthe planet.The Viking 1 and Viking 2 lander missions were designed to address the question

of extant (rather than extinct) life on Mars (see Chapter 5). Three experiments wereselected to detect metabolic activity, such as photosynthesis, nutrition, and respi-ration of potential microbial soil communities. The results were ambiguous,because although “positive” results were obtained, no organic carbon was foundin the Martian soil by gas chromatography–mass spectrometry (GC-MS). It wasconcluded that the most plausible explanation for these results was the presence atthe Martian surface of highly reactive oxidants, such as hydrogen peroxide, whichwould have been photochemically produced in the atmosphere. Direct photolyticprocesses were suggested to be responsible for the degradation of organics at theMartian surface. Because the Viking landers could not sample soils below 6 cm, thedepth of this apparently organic-free and oxidizing layer is still unknown. Moreinformation is expected from the upcoming lander missions to Mars: the U. S.Mars Science Laboratory (MSL) to be launched in 2009 and the European ExoMarsmission to be launched in 2013 (see Chapter 12).There are Martian rocks on Earth represented by a small group of meteorites of

igneous (volcanic) origin, known as the SNCmeteorites (after their type specimensShergotty, Nakhla, and Chassigny), that had comparatively young crystallizationages, equal to or less than 1.3 billion years (see Chapter 8). One of these meteorites,designated EETA79001, was found in Antarctica in 1979. It had gas inclusionstrapped within a glassy component. Both compositionally and isotopically, this gasmatched the makeup of the Martian atmosphere, as measured by the Viking massspectrometer. The data provide a very strong argument that at least that particularSNC meteorite came from Mars, representing the product of a high-energy impactthat ejected material into space. There are now 34 SNC meteorites known in total.Two of the SNC meteorites, EETA79001 and ALH84001, supply new and highly

interesting information. A subsample of EETA79001, excavated from deep withinthe meteorite, has been subjected to stepped combustion. The CO2 release from200–400�C suggested the presence of organic molecules. The carbon is enriched in12C, and the carbon isotope difference between the organic matter and the carbo-nates in Martian meteorites is greater than that observed on Earth. This could beindicative of biosynthesis, although some as yet unknown abiotic processes couldperhaps explain this enrichment. David McKay has reported the presence of otherfeatures in ALH84001 that may represent a signature of relic biogenic activity onMars, but this biological interpretation is strongly questioned.

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Because Mars had a presumably “warm” and wet past climate, it should havesedimentary rocks deposited by running and/or still water on its surface as well aslayers of regolith generated by impacts. Such consolidated sedimentary rockstherefore ought to be found among the Martian meteorites. However, no suchsedimentary material has been found in any SNCmeteorite. It is possible that theydid survive the effects of the escape acceleration from the Martian surface but didnot survive terrestrial atmospheric entry because of decrepitation of the cementingmineral. The “STONE” experiment, flown by ESA, was designed to study preciselysuch physical and chemical modifications to sedimentary rocks during atmospher-ic entry from space (see Chapter 11). A piece of basalt (representing a standardmeteoritic material), a piece of dolomite (sedimentary rock), and an artificialMartian regolith material (80% crushed basalt and 20% gypsum) were embeddedinto the ablative heat shield of the satellite Foton 12, which was launched on 9September 1999 and landed on 24 September 1999. Such an experiment had neverbeen performed before, and the samples, after their return, were analyzed for theirchemistry, mineralogy, and isotopic compositions by a European consortium.Atmospheric entry modifications are made visible by reference to the untreatedsamples. The results suggest that some Martian sedimentary rocks might, in part,survive terrestrial atmospheric entry from space.Even if convincing evidence for ancient life in ALH84001 has not been estab-

lished, the two SNCmeteorites (EETA79001 and ALH84001) do show the presenceof organic molecules. This suggests that the ingredients required for the emer-gence of primitive life were present on the surface of Mars. Therefore, it istempting to consider that microorganisms may have developed on Mars and livedat the surface until liquid water disappeared. Because Mars probably had no platetectonics, and because liquid water seems to have disappeared from Mars’ surfacevery early, theMartian subsurface perhaps keeps a frozen record of very early formsof life.Currently, a very intensive exploration of Mars is planned, and U. S., European,

Russian, and Japanese missions to Mars are taking place or are in the planning.Exobiology interests are included, especially in the analysis of samples from siteswhere the environmental conditions may have been favorable for the preservationof evidence of possible prebiotic or biotic processes. The European Space Agency(ESA) convened an Exobiology Science Team chaired by this author to design anintegrated suite of instruments to search for evidence of life on Mars. Priority wasgiven to the in situ organic and isotopic analysis of samples obtained by subsurfacedrilling. The basic recommendations of the Exobiology Science Team are presentlyserving as guidelines for the elaboration of the Pasteur exobiology payload of theESA ExoMars mission scheduled for 2013 (see Chapter 12).

1.4.2Jupiter’s Moon Europa

The Jovian moon Europa appears as one of the most enigmatic of the Galileansatellites. With a mean density of about 3.0 g cm–3, the Jovian satellite should be

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dominated by rocks. Ground-based spectroscopy, combined with gravity data,suggests that the satellite has an icy crust, which is kilometers thick, and a rockyinterior. The images obtained by the Voyager spacecraft in 1979 showed very fewimpact craters on Europa’s surface, indicating recent, and probably continuing,resurfacing by cryovolcanic and tectonic processes. Recent images of Europa’ssurface, taken by the Galileo spacecraft over 14 months (from December 1997 toDecember 1999), show surface features – iceberg-like rafted blocks, cracks, ridges,and dark bands – that are consistent with the presence of liquid water beneath theicy crust. Data from Galileo’s near-infrared mapping spectrometer show hydratedsalts that could be evaporites. The most convincing argument for the presence ofan ocean of liquid water comes from Galileo’s magnetometer. The instrumentdetected an induced magnetic field within Jupiter’s strong magnetic field. Thestrength and response of the induced field require a near-surface, global conduct-ing layer, most likely a layer of salty water (see Chapter 10).If liquid water is present within Jupiter’s moon Europa, it is quite possible that it

includes organic matter derived from thermal vents. Terrestrial-like prebioticorganic chemistry and primitive life may therefore have developed in Europa’socean. If Europa maintained tidal and/or hydrothermal activity in its subsurfaceuntil now, it is possible that microbial activity is still present. Thus, the possibilityof extraterrestrial life present in a subsurface ocean of Europa must seriously beconsidered. The most likely sites for extant life would be at hydrothermal ventsbelow the most recently resurfaced area. To study this directly would requiremaking a borehole through the ice in order to deploy a robotic submersible. Onthe other hand, biological processes in and around hydrothermal vents couldproduce biomarkers that would be pushed up as traces in cryovolcanic eruptionsand thereby be available at the surface for in situ analysis or sample return. Mineralnutrients delivered through cryovolcanic eruption would make the same locationsthe best candidates for autotrophic life.

1.4.3Saturn’s Moon Titan

Titan’s atmosphere was revealed mainly by the Voyager 1 mission in 1980, whichyielded the bulk composition (90% molecular nitrogen and about 1–8% methane).Also, a great number of trace constituents were observed in the form of hydro-carbons, nitriles, and oxygen-containing compounds, mostly CO and CO2. Titan isthe only other object in our Solar System bearing any resemblance to our own planetin terms of atmospheric pressure, which amounts to 1.5 105 Pa (1.5 bar), andcarbon/nitrogen chemistry. It therefore represents a natural laboratory for studyingthe formation of complex organic molecules on a planetary scale and over geologicaltimes (see Chapter 9). The European Space Agency’s Infrared Space Observatory(ISO) has detected tiny amounts of water vapor in the higher atmosphere, but Titan’ssurface temperature (94 K) is much too low to allow the presence of liquid water.Although liquid water is totally absent at the surface, the satellite provides a uniquemilieu to study, in situ, the products of the fundamental physical and chemical

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interactions driving a planetary organic chemistry. Herewith, Titan serves as areference laboratory to study, by default, the role of liquid water in exobiology.The NASA–ESA Cassini–Huygens spacecraft launched in October 1997 arrived in

the vicinity of Saturn in 2004 and performed several flybys of Titan, makingspectroscopic, imaging, radar, and other measurements. On 14 January 2005, aninstrumented descent probe managed by European scientists penetrated the at-mosphere and systematically studied the organic chemistry in Titan’s geofluid. For150 min, in situmeasurements provided analyses of the organics present in the air,in the aerosols, and at the surface. The GC-MS of theHuygens probe measured thechemical composition and the isotopic abundances, from an altitude of 140 kmdown to the surface. The main findings are as follows:

• nitrogen and methane are the main constituents of theatmosphere;

• the isotopic ratio 12C/13C suggests a permanent supply ofmethane in the atmosphere;

• the surface is “wetted” by liquid methane and rich in organics(cyanogen, ethane);

• the presence of 40Ar suggests the existence of internalgeological activity.

1.5The Search for Life Beyond the Solar System

1.5.1The Search for Rocky Earthlike Exoplanets

Apart from abundant hydrogen and helium, 114 interstellar and circumstellargaseous molecules have been identified in the interstellar medium (see Chapter 2).It is commonly agreed that the catalog of interstellar molecules represents only afraction of the total spectrum of molecules present in space, the spectral detectionbeing biased by the fact that only those molecules possessing a strong electricdipole can be observed. Among these molecules, 83 contain carbon, whereas only 7contain silicon. Silicon has been proposed as an alternative to carbon as the basis oflife. However, silicon chemistry is apparently less inventive and does not seem tobe able to generate any life as sophisticated as the terrestrial carbon-based one. Maythese molecules survive the violent accretion phase generating a planetary system?The origin and distribution of the molecules from the interstellar medium to the

planets, asteroids, and comets of the Solar System are presently at the center of adebate based on isotope ratios. Some molecules might have survived in coldregions of the outer Solar System, whereas others would have been totally reproc-essed during accretion. Whatever the case, the interstellar medium tells us thatorganic chemistry is universal.What about liquid water? New planets have been discovered beyond the Solar

System. On 6 October 1995, the discovery of an extrasolar planet, i.e., a planet

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outside our Solar System, was announced byMichel Mayor and Didier Queloz. Theplanet orbits an 8 billion year old star called 51 Pegasus, 42 light years away withinthe Milky Way. The suspected planet takes just four days to orbit 51 Pegasus. It hasa surface temperature around 1000�C and a mass about 0.5 the mass of Jupiter.One year later, seven other extrasolar planets were identified. Among them, 47Ursa Major has a planet with a surface temperature estimated to be around that ofMars (–90 to –20 �C), and the 70 Virginis planet has a surface temperatureestimated at about 70–160 �C. The latter is the first known extrasolar planet whosetemperature might allow the presence of liquid water. As of May 2006, 193exoplanets had been observed.

1.5.2Detecting Extrasolar Life

Extrasolar life, i.e., life on a planet of a solar system other than our own, will not beaccessible to space missions in the foreseeable future. The formidable challenge ofdetecting distant life must therefore be tackled by astronomers and radio astron-omers. The simultaneous detection of water, carbon dioxide, and ozone (an easilydetectable telltale signature of oxygen) in the atmosphere would constitute themost convincing biomarker but not absolute proof. Other anomalies in the atmos-pheres of telluric exoplanets (i.e., rocky Earthlike planets), such as the presence ofmethane, might be the signature of an extrasolar life. European astrophysicists areproposing the construction of a flotilla of four free-flying spacecrafts, each con-taining an infrared telescope of 3 m in diameter, to search for signs of life onterrestrial-like planets. The mission, called Darwin-IRSI, is presently under studyat ESA. Finally, the detection of an unambiguous electromagnetic signal (via theSearch for Extraterrestrial Intelligence program) would obviously be an excitingevent.

1.6Conclusions

On Earth, life probably appeared about 4 billion years ago, when some assemblagesof organic molecules in a liquid water medium began to transfer their chemicalinformation and to evolve by making a few accidental transfer errors. The numberof molecules required for those first assemblages is still unknown. The problem isthat on Earth, those molecules have been erased. If life started on Earth with theself-organization of a relatively small number of molecules, its emergence musthave been fast; therefore, the chance of the appearance of life on any appropriatecelestial bodies might be real. On the other hand, if the process required thousandsof different molecules, the event risks being unique and restricted to the Earth.The discovery of a second independent genesis of life on a body presenting

environmental conditions similar to those prevailing on the primitive Earth wouldstrongly support the idea of a rather simple genesis of terrestrial life. More than

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just a societal wish, the discovery of a second genesis of life is a scientific need forthe study of the origin of life. It will demonstrate that life is not a magic, one-shotprocess but a rather common phenomenon. Many scientists are convinced thatmicrobial life is not restricted to the Earth, but such conviction now needs to besupported by facts.

1.7Further Reading

1.7.1Books and Articles in Books

Brack, A. (Ed.) The Molecular Origins of Life:Assembling Pieces of the Puzzle, CambridgeUniversity Press, Cambridge, 1998.

Gilmour, I., Sephton, M. A. (Eds.) An Intro-duction to Astrobiology, The Open Universityand Cambridge University Press, Cam-bridge, 2003.

Clancy, P., Brack, A., Horneck, G. Looking forLife. Searching the Solar System, CambridgeUniversity Press, Cambridge, 2005.

De Duve, C. Possible starts for primitive life.Clues from present-day biology: the thioest-er world, in: A. Brack (Ed.) The MolecularOrigins of Life: Assembling Pieces of the Puzzle,Cambridge University Press, Cambridge,pp. 219–236, 1998.

Fox, S.W. Dose, K. Molecular Evolution and theOrigin of Life (Revised Edition), MarcelDekker, New York, 1977.

Gargaud, M., Barbier, B., Martin, H., J. Reisse,J. (Eds.) Lectures in Astrobiology, Springer-Verlag, Berlin, Heidelberg, 2005.

Horneck. G., Baumstark-Khan, C. (Eds.)Astrobiology – The Quest for the Conditions ofLife, Springer, Berlin, Heidelberg, NewYork, 2002.

Jakosky, B. The Search for Life on Other Planets,Cambridge University Press, 1998.

Jones, B.W. (Ed.) Life in the Solar System andbeyond, Springer, Berlin, Heidelberg, NewYork 2004.

Maurette, M. Micrometeorites and the Mysteriesof our Origins, Springer, Berlin Heidelberg,New York, 2006.

Rauchfuss, H. Chemische Evolution, Springer,Berlin, Heidelberg, New York, 2005

Schulze-Makuch, D., Irwin L. N. Life in theUniverse, Springer, Berlin, Heidelberg, NewYork, 2004.

Westall, F., Southam, G. The early record oflife, in: K. Benn, J.-C. Mareschal, K. C.Condie (Eds.) Archean Geodynamics and En-vironments, American Geophysical Union,Washington DC, pp. 283–304, 2006.

1.7 Further Reading 21

1.7.2Articles in Journals

Boillot, F., Chabin, A., Bur�, C., Venet, M.,Belsky, A., Bertrand-Urbaniak, M., Delmas,A., Brack, A., Barbier, B. The Perseus exo-biology mission on MIR: behaviour of ami-no acids and peptides in Earth orbit, OriginsLife Evol. Biosphere 2002, 32, 359–385.

Brack, A. From amino acids to prebiotic activepeptides: a chemical reconstitution, PureAppl. Chem. 1993, 65, 1143–1151.

Brack, A., Baglioni, P., Borruat, G., Brandst�t-ter, F., Demets, R., Edwards, H. G.M.,Genge, M., Kurat, G., Miller, M. F., Newton,E.M., Pillinger, C. T., Roten, C.-A., W�sch,E. Do meteoroids of sedimentary originsurvive terrestrial atmospheric entry? TheESA artificial meteorite experiment STONE,Planet. Space Sci. 2002, 50, 763–772.

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Cronin, J. R., Pizzarello, S. Enantiomeric ex-cesses in meteoritic amino acids, Science1997, 275, 951–955.

Deamer, D.W. Boundary structures areformed by organic components of theMurchison carbonaceous chondrite, Nature1985, 317, 792–794.

Eschenmoser, A. Chemical etiology of nucleicacid structure, Science 1999, 284, 2118–2124.

Ferris, J. P., Hill, A. R. Jr, Liu, R., Orgel, L. E.Synthesis of long prebiotic oligomers onmineral surfaces, Nature 1996, 381, 59–61.

Luther, A., Brandsch, R., von Kiedrowski, G.Surface-promoted replication and exponen-tial amplification of DNA analogues, Nature1998, 396, 245–248.

Maurette, M., Duprat, J., Engrand, C., Gou-nelle, M., Kurat, G., Matrajt, G., Toppani, A.Accretion of neon, organics, CO2, nitrogenand water rom large interplanetary dustparticles on the early, Earth Planet. Space Sci.2000, 48, 1117–1137.

Mayor, M. D., Queloz, D. A. Jupiter-masscompanion to a solar-type star, Nature 1995,378, 355–359.

Miller, S. L. The production of amino acidsunder possible primitive Earth conditions,Science 1953, 117, 528–529.

Munoz Caro, G.M., Meierhenrich, U. J.,Schutte, W. A., Barbier, B., Arcones Segovia,A., Rosenbauer, H., Thiemann, W.H.-P.,Brack, A., Greenberg, J. M. Amino acidsfrom ultraviolet irradiation of interstellar iceanalogues, Nature 2002, 416, 403–405.

Niemann, H.B et al. The abundances of con-stituents of Titan’s atmosphere from theGC-MS instrument on the Huygens probe,Nature 2005, 438, 779–784.

Ogata, Y., Imai, E.-I., Honda, H., Hatori, K.,Matsuno, K. Hydrothermal circulation ofseawater through hot vents and contributionof interface chemistry to prebiotic synthesis,Origins Life Evol. Biosphere 2000, 30, 527–537.

Ourisson, G., Nakatani, Y. The terpenoidtheory of the origin of cellular life: the evo-lution of terpenoids to cholesterol, Chem.Biol. 1994, 1, 11–23.

Paecht-Horowitz, M., Berger, J., Katchalsky, A.Prebiotic synthesis of polypeptides by het-erogeneous polycondensation of amino-acidadenylates, Nature 1970, 228, 636–639.

Pizzarello, S., Cronin, J,R. Non-racemic ami-no-acids in the Murray and Murchison me-teorites, Geochim. Cosmochim. Acta 2000,64(2), 329–338.

Schmidt, J. G., Nielsen, P. E., Orgel, L. E.Information transfer from peptide nucleicacids to RNA by template-directed synthe-ses, Nucleic Acids Res. 1997, 25, 4797–4802.

Schçning, K.-U., Scholz, P., Guntha, S., Wu,X., Krishnamurthy, R., Eschenmoser, A.Chemical etiology of nucleic acid structure:the Æ-threofuranosyl-(3’2’) oligonucleotidesystem, Science 2000, 290, 1347–1351.

Schopf, J. W. Microfossils of the Early ArcheanApex Chert: new evidence of the antiquity oflife, Science 1993, 260, 640–646.

Severin, K. S., Leem, D.H., Martinez, J. A.,Ghadiri, M. R. Peptide self-replication viatemplate-directed ligation, Chem. Eur.J.1997, 3, 1017–1024.

Terfort, A., von Kiedrowski, G. Self-replicationby condensation of 3-aminobenzamidinesand 2-formyl-phenoxyacetic acids, Angew.Chem. Int. Ed. Engl. 1992, 31, 654–656.

W�chtersh�user, G. Life in a ligand sphere,Proc. Natl. Acad. Sci. USA 1994, 91, 4283–4287.

Westall, F. Life on the early Earth: a sedimen-tary view, Science 2005, 308,366–337.

Wintner, E. A., Conn, M.M., Rebek, J. Studiesin molecular replication, Acc. Chem. Res.1994, 27, 198–203.

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1.7.3Web Sites

Jet Propulsion Laboratory / NASA: Mars Mete-orites, 2003 http://www.jpl.nasa.gov/snc/

Schneider, J. 2003. http://www.obspm.fr/encycl/f-encycl.html.

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2From the Big Bang to the Molecules of LifeHarry J. Lehto

This chapter deals with the evolution of the Universe that predatesboth chemical evolution and the evolution of life. First, the originof the elements critical for life is reviewed. The origin of hydrogenand helium is explained from cosmological models. Hydrogen isrequired when water is formed. Helium, which appears quiteuseless for life, turns out to be critical in the stellar synthesis ofcarbon leading to heavier elements. The second constituent ofwater, oxygen, is also formed in the hot cores of stars. Once theseelements are expelled from stars back into the cool interstellarspace, they get mixed into the interstellar clouds resulting in a vastspectrum of molecules. The observed properties of these moleculesand of the larger dust particles are reviewed. They play an impor-tant role in the formation of planets in the accretion disks of metal-rich populations of stars. This material, which is reprocessed by thenewly formed stars and other planets in the planetary system,“rains” on the young planet in the form of meteorites, comets, andasteroids, creating a supply of raw materials for the prebioticevolution and the eventual biological evolution of life. Theseprocesses are considered in the light of the formation of the Earth.

2.1Building Blocks of Life

Life as we know it is made of compartments, the cells. Within all cells similarmolecules are found, no matter which cell is considered.

• Water (H2O) is the basis for the cytoplasm of all cells: all theessential biological reactions take place in water. Water is alsoessential for transport of nutrients and waste. The elementsin water are quite obviously hydrogen (H) and oxygen (O) (seeChapter 1).

• Nucleic acids (DNA and RNA) are essential to present lifeforms in providing instructions on how to build proteins and

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in transferring this information from one generation of cellsto the next. Nucleic acids are long polymers that consist ofnucleotide bases – cytosine, guanine, thymine, and adeninein DNA and cytosine, guanine, uracil, and adenine in RNA –joined by a backbone formed by a sugar – deoxyribose in DNAor ribose in RNA containing five carbon atoms – and aphosphate group, connecting the adjacent sugars. The ele-ments found in the nucleic acids are carbon (C), H, nitrogen(N), O, and phosphorus (P) (see Chapters 3 and 4).

• Amino acids are the building blocks of proteins. They are alsoquite complex molecules that are exclusively made of C, H, N,O, and sulfur (S) (see Chapter 3).

• Lipids are the fundamental molecules in cellular membranes.Normally, membranes are bi-layered with water-attracting(hydrophilic) layers on the outside and water-repelling (hy-drophobic) layers in the “internal” layers. The hydrophobiclayers are hydrocarbon chains, and the hydrophilic endsusually contain phosphate groups. The main elements inlipids are C and H, but O, N, and P are also used in thehydrophilic ends.

• Carbohydrates, comprising sugars, starches, collagens, orcellulose, are important for all life forms. Carbohydrates areenergy-rich compounds that function as energy-storage andstructural compounds in cells. On the first level, they areproduced by autotrophic life forms by reducing CO2, either byusing energy derived from geochemical compounds or bybinding solar energy. The sugars deoxyribose and ribose playan essential role in forming the backbone of the DNA andRNA. The essential elements in carbohydrates are C,H, andO.

During the dawn of life the prebiotic formation of these complex molecules tookplace through simpler precursor molecules. These are most likely H2O, form-aldehyde (H2CO), hydrogen cyanide (HCN), small sugars (CH2O)n, ammonia(NH3), methane (CH4), and other hydrocarbons –(CH2)n– (see Chapter 3).Six elements, namely C, H, O, N, S, and P, make up 98% of all living tissue. They

are the most important elements of known life. The remaining 2% of living tissueis made of other elements. The exact list of trace elements differs somewhat amongauthors. There is common agreement that the most important trace elements aresodium (Na), chlorine (Cl), potassium (K), fluorine (F), calcium (Ca), iodine (I),magnesium (Mg) and iron (Fe). Ca and F are needed for external skeletons; K, Na,Cl, and I for nervous systems; and Mg and Fe for chlorophyll and hemoglobin,respectively. K, Na, and Cl are needed for maintaining the correct osmotic pressureof cells.Some authors suggest a list of less important trace elements, such as boron (B),

aluminum (Al), silicon (Si), chromium (Cr), manganese (Mn), copper (Cu), zinc

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(Zn), selenium (Se), strontium (Sr), molybdenum (Mo), silver (Ag), tin (Sn), lead(Pb), nickel (Ni), bromine (Br), and vanadium (V). Other authors would removesome elements or add some other ones. The need for specific trace elementsdepends on the species and its environment.In summary, one may conclude that approximately 25–30 elements are needed

for life. The remaining 80 elements are not essential and often turn out to bedetrimental to life.

2.2Big Bang: Formation of H and He

At the beginning, the Universe was small, dense, and hot and there were noelements. What happened during the first 10–43 seconds is beyond the realm ofphysics. At 10–43 seconds the temperature was 1019 GeV (for convenience, 1 eV k–1

~11 605 K, so 1 GeV corresponds to 1013 K; k is the Boltzmann constant). Hence,1019 GeV corresponds to a temperature of 1032 K, a number so high that it is hard toimagine.When considering the evolution of the early Universe, the single most important

parameter is temperature. The physics of the early Universe is easiest to under-stand in terms of temperature because equations of state of its different compo-nents are most conveniently calculated as a function of temperature. The begin-ning of the Universe took place some 13.7 € 0.15 billion years ago. The Universestarted to expand immediately (Fig. 2.1).The Universe was dominated by radiation. Elementary particles changed con-

tinuously to radiation and vice versa. At 10 GeV, when 0.01 �s had elapsed,particles called bosons started to decouple from radiation; protons, neutrons,and mesons began to form. This continued until temperature fell to about100 MeV (1012 K), when the temperature of the Universe became too low for theformation of these particles. At this point all protons, neutrons, and mesons wereformed. In the meantime, about 100 �s had elapsed. Later, the protons wouldbecome the nuclei of hydrogen atoms, and neutrons and protons would combine toform alpha particles or helium nuclei. The Universe continued expanding and itstemperature fell.Within the next second the temperature fell enough for the formation of

electron-positron pairs. Most of these pairs annihilated back to radiation, butbecause of an antimatter-matter symmetry, a surplus of electrons was left.For astrobiology, the next relevant moment in the evolution of the Universe was

the time of nucleosynthesis. It started at about 1 s from the beginning, when thenumber of photons in the Universe, with energies smaller than 2.2 MeV, corre-sponding to the binding energy of a deuteron (proton + neutron) fell below thenumber of neutrons. The nucleosynthesis continued for about 5 min, until thetemperature fell to about 70 keV (or 8 � 108 K). The number of neutrons duringthis era was such that there was 1 neutron (nn) for 7 protons (np). This fixed themass ratio of helium (He) to hydrogen (H) at:

2.2 Big Bang: Formation of H and He 25

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2 nnnp

� �

1þ nnnp

� � ¼ 14

(2.1).

At that time, almost all neutrons became bound to He. In addition, some lightnuclei lithium (Li), B, and beryllium (Be), as well as 3He and deuterium (D), wereformed around this time. Heavier nuclei did not form because there are no stablefive-nucleon nuclei and because heavier nuclei would have required the presence ofHe nuclei and even higher temperatures. Within the next few minutes, the Henuclei were formed, and the last remaining neutrons decayed with a half lifetime of615 s (or a mean lifetime of 886 s).When the temperature of the Universe fell to T = 0.8eV or 9284 K (t = 47 000

years) it was time for photons to decouple from matter. The Universe became

2 From the Big Bang to the Molecules of Life26

Fig. 2.1 Evolution of the early Universe (Image credit: ESA).

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matter dominated. Relatively soon, at T = 0.3 eV or 3 000 K, or 380 000 years fromthe Big Bang, the average background photon encountered its last scattering.The distant faint glow of the temperature (and matter) fluctuations of that

moment can be seen as the cosmic microwave background. Around the time ofthe last scattering, the temperature had fallen enough so that atoms could alsoform. Protons combined with electrons into H, and two electrons and an alphaparticle formed He atoms. The scale factor (a sort of a measure of size) of theUniverse at the time was about 0.09% of the present value.The production of light elements in the Big Bang was first calculated in 1948 by

Ralph Alpher, Hans Bethe and George Gamow. They predicted a microwavebackground radiation of 5 K. This basic idea was then confirmed in 1964 by theNobel-winning, serendipitous observations of background radiation by Penziasand Wilson. They measured the temperature to be 3 K. More recently, in 1990, theobservations from the NASA satellite Cosmic Background Explorer (COBE) showedthat the radiation spectrum of the cosmic microwave background follows veryaccurately a blackbody spectrum.In 2003, the Wilkinson Microwave Anisotropy Probe (WMAP) team led by Charles

Bennett from John Hopkins University provided the best fit to the temperature ofthe microwave background, with a temperature of T = 2.725 € 0.002 K. Theseobservations were further analyzed by subtracting from each point the averagespectrum of the sky and by removing the dipole component, which is at a level ofabout 3 mK and is caused by our movement with respect to the microwave back-ground. In addition, the galactic contribution to the background was removed –this is radiation found mostly on the galactic plane. One was left with temperaturefluctuations frozen to the background at the time of the last scattering. They showup as tiny ˜T ~10–5 K fluctuations in the background. By measuring the correla-tions in these fluctuations over different angular scales over the whole sky down toabout 0.3 degree, one can calculate a two-point correlation function. This can thenbe compared to various cosmological models.The model that best explains the observed distribution is a Universe that

experienced a rapid expansion or inflation starting at 10–35 s from the beginningand lasting for 10–32 s. Furthermore, the present conditions of the Universe aresuch that it is expanding at a rate of a Hubble constant, which has ameasured valueof H = 71 € 2 km s–1 Mpc–1 (pc = parsec, a unit of astronomical length, with1 pc » 3 � 1016 m). The average density of the Universe is equal to the criticaldensity within a measurement error of 2%. The critical density is the averagedensity of the Universe at which the geometry of the Universe is flat:

æ ¼ 3H2=8�G � 1:0� 10�26g cm–3, (2.2),

where H = Hubble constant and G = gravitational constant.The observed statistical properties of the microwave background have been

explained by invoking the presence of dark energy. Mathematically, this corre-sponds to the cosmological constant, which was introduced to the standard Fried-man equations by Albert Einstein. He did not like the idea that the Universe could

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be non-static and added ad hoc his cosmological constant. For decades, thisconstant was considered a curiosity, but now, with the latest microwave data, ithas become quite useful again.About 73% of the energy density in the Universe is in the form of dark energy. At

present it is not knownwhat this is physically or theoretically, but it can bemathemati-cally understood as the energy density of vacuum. Its presence is also suggested by theaccelerating expansion rate detected from observations of supernovae and some otherobservations. The remaining 27% of the energy density is matter. About 85% of thismatter is “dark matter.” The physical nature of this matter is not yet known, but itsinfluence can be seen, e.g., in orbits of stars in galaxies or in the velocity dispersion ofgalaxies in galaxy clusters. The remaining matter (15% of matter and 4% of the totalenergy density) is baryonicmatter,mainlyH andHe.Heavier elements constitute 1%of the combined H and He mass only. Thus, assuming that the dark energy is real,only about 0.04%of the density of theUniverse is in the formof heavier elements suchas C, N, O, or Fe, which are the elements life is made of (Fig. 2.2).

2.3First Stars: Formation of Small Amounts of C, O, N, S and P andOther Heavy Elements

After the last scattering of the photons, a dark era followed in the Universe(Fig. 2.1). No stars existed for another 100–300 million years. It took about thattime for the first gas clouds to collapse and form the first stars. The details of thephysics of those stars and the exact timescales of their formation and evolution arestill unclear. Using the Spitzer Space Telescope, faint infrared (IR) fluctuations in thecosmic IR background were measured by Kashlinsky and his collaborators in late2005. They argue that the fluctuations are caused by combined light from a largenumber of the very first stars. No individual stars are seen. The ultraviolet (UV)

2 From the Big Bang to the Molecules of Life28

Fig. 2.2 Components of the Universe. Darkenergy: 73%; cold dark matter: 23%; baryonicmatter, which is mostly H and He: 4%; neutri-nos: 0.3% (dark gray sector); heavier elementssuch as O, C, and N: 0.04% (white sector). Thelast sector is the sector of life.

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emission from the stars is now observed as highly red-shifted radiation in the IR.This radiation could well come from the very first stars.It is likely that these are the only stars that formed along the lines first described

by Jeans in 1902. A gas cloud, which was at that time made of H and He, started tocollapse under its own weight. The collapse is initiated if the mass of the cloud islarger than the Jeans’ mass:

Mcloud> MJM = 700 M� (T / 200 K)1.5 (n / 106)–0.5 (2.3),

where n = the number density of particles (H andHe) per cm3, T = the temperatureof the cloud in K, andM� = the solar mass, a basic mass unit in many astronomicalcalculations.Thus, if the cloud has a density of n = 106 cm–3 and a temperature of T = 200 K,

then a cloud exceeding a mass of 700 M� would be able to collapse. If the temper-ature is higher than T = 200 K, then the cloud should be more massive for the totalgravitational attraction to overcome the added pressure caused by the increasedtemperature. Similarly, if the gas density is higher than n = 106 cm–3, then asmaller cloud could collapse according to this model.As the collapsing proceeds, the density in the cloud center increases. With the

increased density the pressure at the center increases, as does the temperature.Finally, in the central 1% or so, the temperature of the cloud rises to 4 � 106 K, andnuclear reactions begin. There appears to be no clear reason for an upper limit ofthe mass of a star formed in this way. It is possible that the very first stars hadmasses of 100–300 M�, or even as large as 500 M�. These very massive stars livedshort lives of only one million years or so and produced the first heavier elements,such as C, N, O, P, S, Al, and Fe. At the end of their lives, they exploded and shed allthese new heavy elements into the surrounding, still quite dark space. These earlystars are now referred to as population III stars. The first galaxies formed when theUniverse had an age of maybe 600–800 million years. All the stars formed in thesenew nascent galaxies have a minutely tiny seed of heavier elements in addition tothe overwhelmingly abundant H and He.

2.4Normal Modern Stars, Bulk Formation of C, O, N, S, P and Other Heavy Elements

Stars can be classified by several different means. The most important classifica-tion scheme is the Hertzsprung-Russell (HR) diagram (Fig. 2.3). A version of theHR diagram, the color magnitude diagram, shows the brightness of the star, e.g., Vmagnitude, as a function of its color, e.g., brightness difference in two bands, saythe blue and visual (B – V). Several variations of this diagram exist. If the distanceto a star is known and its apparent brightness is measured, then its luminosity canbe calculated. If a spectrum of the very same star also can be obtained, then thetemperature of its photosphere can be determined. By doing this to a multitude ofstars, an HR diagram in a form that is more relevant to astrobiology can be drawn.

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Here, the brightness of the star, given as logarithm of luminosity, is plotted againstthe logarithm of temperature.If the star is assumed to behave like a perfect blackbody radiator, which is a

reasonable assumption in this context, then straight lines of constant stellar radiican be drawn into this plot. Furthermore, if the luminosity and the temperature ofthe central star are known, the distance of the habitable zone can be included inthis same plot. This is shown in Fig. 2.4 on the right. This assumes the definition ofa habitable zone, put forward by Kasting, as the region around the star where thetemperature is such that water stays liquid (see Chapter 6). The lower edge of thistemperature range is close to 0ºC at a range of pressures, but the higher enddepends on the atmospheric pressure of the planet itself. At 105 Pa (1 atm) it is100 �C, but at 2 � 105 Pa it is 121 �C.Because habitability depends on the luminosity of the central star, the distance of

the habitable zone is set on approximately horizontal lines on the diagram. Consid-

2 From the Big Bang to the Molecules of Life30

Fig. 2.3 Schematic representation of a Hertz-sprung-Russell (HR) diagram; it shows the startemperature or spectral type as abscissa andstar luminosity or absolute magnitude asordinate. Temperature of stars decreases from

left to right with the spectral type sequence ofstars: O, B, A, F, G, K, M, to L. The diagonallines at 100, 1, and 0.01 represent theapproximate radius of the star in solar radii.

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ering the limitations, several areas of the HR diagram can be ruled out as ratherunsuitable for life. Even the most optimistic views of habitability can be condensedinto a triangle (Fig. 2.4). Thismay be an area where life could, in principle, form. Forlife to evolve to a higher evolutionary stage, the conditions on the central star shouldstay relatively stable for at least one billion years. This would narrow the starssuitable for life as we know it down to a narrow ellipse-like zone (Fig. 2.4).There is one additional stellar property that is relevant to astrobiology not shown

in the HR diagram. It is what astronomers call metallicity (Z), which is the massfraction of elements heavier than hydrogen and helium. Solar metallicity abun-dance is about 1–2%. Hot, bright stars tend to have high metallicity and faint redstars usually have low metallicity. However, this may not represent a propercorrelation but rather a manifestation of the age of the average star of these spectralclasses. Blue, bright stars are short-lived, but faint red stars are of very differentages, including some that are almost as old as the Universe.The young stars are called population I stars, and the old ones are called

population II stars. Our Sun is a population I star. The different populations ofstars have different roles in astrobiology.

2.4 Normal Modern Stars, Bulk Formation of C, O, N, S, P and Other Heavy Elements 31

Fig. 2.4 Biological HR diagram; lines of a typicaldistance of the habitable zone (HZ) are shown onthe right of the diagram (scaling that of the Sun atHZ = 1.0). Because the range of the HZ dependson the luminosity of the central star, the distances

areset on approximately horizontal lines on thediagram. The triangle (dashed line) describesthe range where life in principle could form. Thenarrow ellipse-like zone describes an area wherelife might evolve to a higher evolutionary stage.

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The first normal stars were formed from very metal-poor gas. There were somemetals around from the very first stars, but the amounts were very low. Even withsuch low concentrations of metals, such as C, the nuclear reactions in stars got animportant boost because these metals are used as catalysts, e.g., in the carbon–nitrogen–oxygen (CNO) cycle. These first normal stars were also the primaryfactories for the heavier elements, which are important for life.The evolution of a single star is determined mainly by its mass. (Binary stars exist

quite commonly, but the theory of binary star evolution will not be considered here.)If the mass of a single object emerging from a collapsing cloud is smaller than about0.08 M�, then its core will not have a high enough temperature to start the fusion ofH into He. If the stellar mass is larger than 0.08 M�, and less than 0.26 M�, thecentral temperature will rise above 4 � 106 K and He production will start at a veryslow pace in the center of the star by the proton–proton chain reaction (p–p chainreaction). Two protons combine to form a deuteron, which then combines with afurther proton to form 3He. Finally, two 3He combine to form a 4He and two protons.The final step can also proceed through a loop involving Li, B, and Be, essentially withthe same end result. This process will continue throughout the lifetime of the star.Stellar models suggest that these stars will stay convective and well mixed. The

same models indicate that their lifetime is in the range of 1011–1013 years. This ismuch longer than the present age of the Universe. None of them have beenwitnessed to “die.” It is thought that after a very long time these stars will endup as white dwarfs. The energy within these stars is transferred via convectionfrom the center of the star through buoyant, hot material rising from the centralparts of the star and cooler material near the surface sinking down.In stars of masses larger than 0.26 M�, elements heavier than He will also form.

Pressure and temperature increase towards the center of a star. It is in the verycenter of the star where most of the nucleosynthesis takes place. The evolution ofstars heavier than about 0.26 M� can be divided into two broad groups with thedividing line at about 1.5 M�.The evolution of a solar type star of mass 0.26 M� < M < 1.5 M� is approximately

as follows. These stars form initially with a central temperature higher than4 � 106 K. The central parts become radiative, while the outer parts stay convective.The p–p chain reaction is the main source of the stellar luminosity for these starsduring the main sequence phase of the star, which lasts about 2–20 billion years.During this time the star is relatively stable. Close to the end of the main sequencephase, the star has developed a helium core that is degenerate, meaning that it isnearly incompressible. Around this core there is a hydrogen fusion envelope thatstarts to expand. The star becomes a red giant.The temperature of the He core increases, until suddenly, when the temperature

reaches about 108 K, the so-called triple-alpha reaction sets in. In this reaction He istransformed into C. Two He nuclei combine into a 8Be nucleus, which is unstable.If a third He nucleus interacts within 3 � 10–16 s, then a 12C nucleus with anemission of a photon results; otherwise, the 8Be decays back to two He nuclei.This reaction requires the near-simultaneous collision of the three He nuclei(alpha particles) and is therefore called the triple-alpha reaction.

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The onset of the triple-alpha reaction across the core is so sudden (few hundredsof seconds) that it causes a He flash, the inner parts of the star collapse, and theouter parts of the star take the extra energy. Later, around the central parts, triple-alpha reactions continue in a He shell. This He shell is surrounded by a H shell,where He is produced by the p–p reaction. The outer envelope expands further, andeventually the star loses the outer shells as an intense stellar wind. A planetarynebula with a hot star in the center results. (It should be emphasized that physicallythe planetary nebula has nothing to do with planets or planetary systems. Thename “planetary nebula” reflects the appearance of these objects as seen byrelatively small telescopes. They tend to look round, not point-like as stars do,and thus are reminiscent of the appearance of planets such as Jupiter or Saturn.)The central star in planetary nebulae is often not visible by small telescopes, butlarge telescopes reveal that the end of the life of a solar mass it to become a whitedwarf. The white dwarf is made mostly of He, but it has a C or O core, and on thesurface it may have a thin outer layer made of H.The gas in the stellar wind during the red giant phase and the planetary nebula

phases consists mainly of H and He, but it also contains about 2% C, N, and O,which are released into the interstellar medium (ISM). Elements heavier than Oare not produced in these stars. Because these lighter stars are substantially morecommon than more massive stars, they have been suggested to be a significantsource of new C, N, and O in the present galaxy.Stars more massive than 1.5 M� have such a high central temperature

(> 18 � 106 K) that a different nuclear fusion mechanism takes over in the con-version of H to He. At these high temperatures the CNO cycle becomes moreeffective than the p–p cycle. One should note that in a CNO cycle, also known as thecarbon cycle, no C is produced; instead, C is needed as a catalyst. The carbon cycleproceeds as follows:

12C + 1H �13N + ª (2.2 a)

13N�13C + e+ + �e (2.2 b)

13C + 1H �14N + ª (2.2 c)

14N + 1H�15O + ª (2.2 d)

15O�15N + e+ + �e (2.2 e)

15N + 1H�12C + 4He (2.2 f)

Reaction (2.2 d) is the slowest one and it determines the total reaction rate. It isimportant to note that this bottleneck creates a surplus of N. Although C is acatalyst in this reaction, it effectively transforms some C into N. Even if the carboncycle is the main source of N in the Universe, the main benefit of this reaction isthe efficient conversion of H into He.

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In these stars the very center of the star will be convective and the outer parts willremain radiative. As in the less massive stars, a He core will eventually form andthe star will become a red giant. Now, however, the He core remains convective,and the onset of He fusion into C by triple-alpha reaction starts at a more leisurelypace; no He flash takes place. A shell-like structure forms, with C in the centersurrounded by He and H shells. Stars in the mass range of 1.5 M� < M < 3 M� willpass through a red giant phase and end up as white dwarfs.The evolution of stars in the range of 3 M� < M < 11 M� is not well understood

theoretically. It appears that in the range of about 3 M� < M < 8 M� the C core willnot ignite and the star will evolve through a red giant phase and end up as a whitedwarf, with the outer parts of the star expelled in a strong stellar wind.In more massive stars (M > 8 M�), the C core will ignite, and a C flash will take

place. Here, the main reaction combines two C, creating an O nucleus and two Henuclei. Later, if the degenerate center has a high enough temperature, two O nucleicombine either into a Mg nucleus and two He nuclei or into one Si and one He. Inthe heaviest stars two Si nuclei combine into one Fe nucleus. All other elementsfrom C to Fe are formed as well. The nuclear reactions producing these elementsare more complex. The conditions at the center of the star will eventually determinewhich are the heaviest nuclei formed. Depending on the mass of the star, an onion-like structure will eventually form with an O, Si, or Fe core. All heavy elements upto Fe and Ni can be formed in these stars as products or side products of the above-mentioned reactions.If the mass of the star is about 8 M� < M < 11 M�, the star will end up with an

O/Ne/Mg core. Thiswill eventually turn into anO/Ne/Mgwhite dwarf, with the outerparts of the star blown out in a fierce stellar wind. Other models suggest that the fateof these stars is to end up as a supernova with a neutron star remnant. In either case,the lighter elements in the outer shells will be expelled into the interstellar space.Stars heavier than about 11 M� have been studied theoretically more extensively.

They will end up with a shell-like structure with Fe in the center, which impliesthat all nuclear fuel in the core has been exhausted. The core will collapse on adynamical timescale, which is on the order of a few hours. The rebounce from thiscollapse will create a shock traveling outwards, resulting in a supernova explosion.The whole mass of the star and all the elements it contains are thrown into thesurrounding space. It is also possible that the center part of the star, the Fe core,will collapse into a black hole or a neutron star, but the outer parts of the star willstill be ejected into space. Supernova explosions have been the main means forliberating the heavier elements into the interstellar space.Elements heavier than Fe are formed in stars in small amounts by the slow

neutron-capture (s) process and in supernovae by the rapid neutron-capture (r)process. These two mechanisms have somewhat different isotope distributions.The heaviest elements formed in the s-process are 208Pb and 209Bi. In the r-processthe heaviest elements are thought to have an atomicmass of about 270. The formationof some rare isotopes such as 190Pt cannot be explained by the s- or r-processes.These are thought to have formed in a supernova explosion by the proton-capture (p)process. Table 2.1 shows a few properties of some main sequence stars.

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Table 2.1 Properties of main sequence stars.

Spectral class Mass (M�) Temperature (K) Age (109 years)

O5 30 44 000 0.005A0 3 12 000 0.24F2 1.5 7 200 2G2 1 5 700 10M0 0.5 3 800 30M7 0.1 2 800 10 000

2.5The First Molecules (CO and H2O)

The most common molecule in the interstellar space is molecular hydrogen (H2).The next most common molecules are carbon monoxide (CO) and water (H2O).These are very interesting molecules because they already contain the heavierelements important for life. The elements making up these molecules were formedin stars that have already ended their life. Walter and coworkers have observed withthe Very Large Array (VLA) situated in New Mexico, USA, the presence of CO inthe spectrum of the quasar SDSS J1148+5251, which has a redshift of z = 6.419.Based on present models of the Universe, this means that these molecules werealready formed 800 millions years after the start of the Universe; thus, at this timethe first ingredients for life were available. The presence of CO indicates thatsubstantial amounts of both C and O had already formed. H2O has not beendetected from this quasar, because of observational limitations, but one can inferits presence because it is formed in a way similar to CO, directly from gaseous Hand O.

2.6Interstellar Matter

Aboriginal Australians see a long, dark emu bird in the sky, with the bonfires oftheir forefathers lighting up the stars of the sky (Fig. 2.5). The “emu” is formed by amultitude of individual dark clouds in the plane of our galaxy. The presence ofinterstellar matter manifests itself also as bright illuminated patches in the skyviewable even with ordinary binoculars. Some of the best examples are Orionnebula M42 and several clouds in Sagittarius and adjacent constellations.The space between stars was thought to be void until Trumpler (1930) noted that

the calculated linear size of open clusters seemed to increase with the distance.Clearly, because such a correlation should not exist, one could reason that distancesto more distant clusters were overestimated. This could only be caused by some

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interstellar dust particles scattering part of the light away on its way from thecluster to our telescopes. At present, it is known that this extinction is on averageabout 2 mmag pc–1 (or 0.06% per light year).The presence of interstellar matter is deduced in several ways. In the optical

region, extinction is one of the most important proofs of interstellar matter. Asecond indication of matter in interstellar space comes from studying two stars thathave similar spectral properties, which means that they have similar intrinsicbrightness and temperature. If one then compares the observed spectrum of themore distant star with that of the closer star, then one can note that it is reddened,which means that light in the blue end of the spectrum is scattered away comparedto the red end of the spectrum. It is a phenomenon similar to that of the reddeningof the Sun as it gets close to the horizon, in which case the scattering is caused bythe tiny O2 and N2 molecules of the atmosphere (Rayleigh scattering). In inter-stellar reddening, the scattering is caused by dust particles in the interstellar space,which are on the order of the wavelength (Mie scattering) in size.The third manifestation of interstellar matter can be observed by studying the

polarization of the starlight. Interstellar dust particles align themselves preferablyalong the feeble galactic magnetic field. As light from a star travels towards us,some light is scattered. Because of the shape of the particles, this scattering has apreferred direction: perpendicular to the longer axis of the particle, meaning thatlight passing through a population of dust particles will have a preferred directionof oscillation, i.e., it will be linearly polarized. By studying this polarization, onemay infer the presence of interstellar non-spherical dust particles and even meas-ure the direction of the galactic magnetic field in different parts of the sky. Bycombining the polarization with the reddening, one obtains the first estimate of thesize and shape of interstellar dust particles.

2 From the Big Bang to the Molecules of Life36

Fig. 2.5 “Emu.” (a) Constellation showing the emu bird in thesky (Photo credit: H. Lehto. La Silla, Chile, 5 March 2006).(b) A real emu bird (Photo credit: H. Lehto, Northern Territory,Australia, 8 August 2003).

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The fourth signature of the presence of intervening interstellar matter are theinterstellar absorption lines in the spectra of stars. Most of the absorption lines instellar spectra are formed in the stellar photosphere, but by studying the Dopplershift and the shape of the individual absorption lines, astronomers can identifyinterstellar lines from the intervening matter and deduce the properties of theinterstellar gas. Note that of the four methods described above, extinction, redden-ing, and polarization measure the properties of the particles, while only one, thespectral absorption lines, indicates the presence of interstellar gas, although themass of the gas outweighs the dust by about 100 to 1.The most common gas in the Universe, H, emits radiation at a wavelength of

21 cm. This radio photon is caused by a small change in the H when the singleelectron orbiting the proton changes its spin direction from being of the oppositesense to being in the same sense as the proton’s spin. Technically speaking, thespin axis changes from antiparallel to parallel. It is very unlikely to happen to asingle atom, as it happens about once in 10 million years, but because there is somuchH along any line of sight, all the added changes shine quite brightly at 21 cm,particularly in the plane of the galaxy. Because practically nothing absorbs thiswavelength, it has proven to be one of the most useful tools in mapping thedistribution of interstellar H in our galaxy. It were these measurements thatshowed that gaseous neutral H (HI) is distributed along spiral arms. Because His the main constituent in the interstellar gas, this study also shows where the bulkof interstellar gas resides. Note that HI refers to neutral H, HII to (singly) ionizedH, and H2 to the molecular H2. All these are important constituents in differentparts of the interstellar medium (ISM).Several different phases of interstellar gas are known, with the coldest and

densest gas being found in molecular gas clouds and the most tenuous and hottestgas, e.g., in supernova remnants. The cold, dense clouds are considered in moredetail in the next section.With the advent of space observatories, extensive IR observations became pos-

sible. These have opened a completely new window for the study of interstellarmatter in its many forms. These observations are discussed in the context of coolinterstellar clouds (Section 2.6.1) and interstellar ice and dust (Section 2.6.3).

2.6.1Interstellar Clouds

The distribution of interstellar dust is not uniform. It is concentrated into inter-stellar clouds that are typically located on the inner edges of the galactic spiralarms. Visually, these clouds appear as dark areas in the sky with much fewer stars;in fact, some of them are optically so opaque that they appear as totally starlesspatches of the sky (Fig. 2.6). Optically, the clouds have such a high extinction thatpractically the only means for studying them is in radio and infrared wavelengths.Spectroscopy in radio wavelengths has two functions. One function is the search

for different molecules. This is done at a large range of wavelengths. From anastrobiological point of view, the most interesting ones are to be found in the

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millimeter ranges. The second function, the spectroscopy of CO, OH, SO, SO2,andother molecules at centimeter and decimeter wavelengths, is critical because itprovides the means for measuring the matter distribution, temperature profiles,and internal motions within the clouds. All this has important implications forunderstanding under which physical conditions complex molecules, dust particles,and ices are formed.IR spectroscopy is the means for studying the properties of dust grains by

looking at signatures of various ices and minerals in the IR emission spectra ofinterstellar clouds. As the extinction in IR is not as severe as in the optical, one canactually recognize at these wavelengths also newborn stars and their accretion

2 From the Big Bang to the Molecules of Life38

Fig. 2.6 Pre-collapse black cloudBARNARD 68. Picture taken by theFocal Reducer/Low Dispersion Spec-trograph (FORS) team on 10 January2001 with the ANTU telescope unit ofthe Very Large Telescope (VLT) locatedon Cerro Paranal in the Atacama Desert,northern Chile (Image credit: EuropeanSouthern Observatory [ESO]).

Fig. 2.7 (a) Orion nebula M42, in the opticalrange. The bright cloud is illuminated by thestars of the Trapezium cluster, which have anage of about 2 million years. (b) Behind theveils of these clouds, a dense molecular cloud

resides, within which hundreds of newlyforming stars are seen in IR. (A: Photo credit:H. Lehto, Tuorla Observatory, Finland, 24January 2004; B: Image credit: ESO).

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disks still surrounded by the blown-away dust shrouds in the depths of the gascloud.The densest of the clouds, the giant molecular clouds (GMC), are completely

opaque at visual wavelengths. The presence of large amounts of H2 is theircharacteristic signature, but they contain also atomic H, inert He, and about 1%of heavier elements. The temperature in the densest parts is 10–20 K. The den-sities, measured in “particles” of mainly H atoms, H2 molecules, and He, can be ashigh as 109 particles per m3, and up to 1012 particles per m3, depending on thecloud. A density of 1012 particles per m3 corresponds to about 10–11 g m–3 or, lessconventionally, 10 mg km–3. For comparison with more familiar units, the densityof the Earth’s air is about 1300 tons km–3. Still, from an astronomical point of view,these clouds are very dense.As an example, one may consider the closest GMC, the Orion cloud. It is at a

distance of about 500 pc and is about 120 pc in extent. From radio and IRobservations, it is known to have an apparent diameter of about 20 degrees inthe sky, or 40 times larger than the moon. One can see the outer edges of the Orioncloud also usually, as the young stars in the Trapezium illuminate the edge of theclouds and create a bright patch known as Orion nebula M42 (Fig. 2.7.A). Thedensest part of the cloud associated with M42 has a diameter of about 25 pc.Examples of the darkness of these clouds can be seen elsewhere in the dense partsof the Orion cloud, e.g., in the dark Horsehead nebula (Fig. 2.8).

2.6.2Interstellar Grains

2.6.2.1 FormationInterstellar grains play a critical role in the formation of interstellar molecules.Interstellar grains are formed mainly in the outer shells of stars when they are intheir red giant or asymptotic giant branch (AGB) phases (M giants, carbon stars, orradio luminous OH/IR stars). Some dust is formed in supernova remnants, novae,

2.6 Interstellar Matter 39

Fig. 2.8 The dark Horsehead nebulain the Orion cloud, observed by theVLT Kueyen and FORS2 (Credit: ESO).

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planetary nebulae, and WC stars and in circumstellar shells around supergiants.The presence of the grains is seen in the opacity caused by the dust and in thermalcontinuum IR emission from the dust. The details of the initial phase of the dustformation, the nucleation, are not well understood. Recent observations suggestthat crystallization of SiO2 takes place directly from the gaseous phase when thetemperature in the stellar wind falls below 700 K. The dust particles grow further inthe tenuous atmospheres of giants and, because of radiation pressure, are drivenaway from the star. The terminal velocity depends on the size of the grain and thematerial – or the mass of the grain. The fastest dispersing grains have a size ofabout 50 �m. Once formed and ejected into the ISM, the dust particles undergovarious kinds of reprocessing, causing both breaking up and growing. The extinc-tion curves observed optically require that a large fraction (>40%) of interstellargrains be >100 nm; therefore, some rebuilding or formation of grains must takeplace in the ISM, possibly in high-density regions by accretion to preexisting graincores.

2.6.2.2 Observed PropertiesIR spectra of ISM show signatures of a population of grains with small radii(a < 10 nm) that absorb about half of the energy emitted by the stars. This radiationis later reemitted in the IR. These grains are believed to be carbonaceous in nature.The smallest of them contain less than 100 C atoms and have tiny sizes (a < 1 nm).They create the IR emission bands characteristic of aromatic carbonaceous rings at3.3 �m, 6.2 �m, 7.7 �m, 8.6 �m, 11.3 �m, and 12.7 �m. The details of the bands arewell explained by a family of large molecules called polycyclic aromatic hydro-carbons (PAHs). Structurally, the molecules are two-dimensional sets of aromaticcarbon rings, consisting of 6 C atoms and each ring connected to each other. The Ccore is surrounded by an outer shell of H atoms. Structurally, the PAHs appearsimilar to pieces of chicken wire made of hexagons. However, precise ground-based laboratory spectra of these molecules are still missing for comparison.Furthermore, a spectral feature at 3.4 �m has been attributed to aliphatic hydro-carbons, which are chain-like in structure.The dust continuum emission in the 25-�m and 60-�m IR bands of the Infrared

Astronomy Satellite (IRAS) has been attributed to slightly larger carbonaceous verysmall grains (1 nm < a < 10 nm). The far-IR continuum radiation is furtherascribed to big grains (a ~ few 10 to few 100 nm), possibly a mixture of largegraphite and silicate grains.Dusty stellar envelopes show broad featureless bands at 10 �m and 20 �m in

both emission and absorption. They have been attributed to amorphous silicates.Recently, additional bands have been observed in the 10–45 �m region. They havebeen attributed to highly ordered crystalline silicates such as Mg-rich olivine(forsterite, Mg2SiO4) or pyroxene (enstatite, MgSiO3). These minerals have notbeen directly seen in spectra of ISM. As a curiosity, a 21-�m IR emission band insupernova remnants has been attributed to tiny diamonds. Their sizes are in therange 0.005–5 �m.

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Depletion of gaseous C, Si, Mg, Fe, and O in ISM suggests that these elementsare used in another phase, possibly as silicates and metal oxides in grains. It shouldbe emphasized that graphite has not been unequivocally detected in the ISM,although it is quite often used as a model.Interstellar matter can be searched for locally in our Solar System. Using isotopic

traces, interstellar grains can be identified in pristine meteorites. They differsomewhat from the particles detected spectroscopically in the ISM. The mostcommon pre-solar grains that have been found are diamonds (2 nm in diameter),SiC (0.05–10 �m), graphite (0.4–6 �m), and Al2O3.High-velocity interstellar particles have been observed in the Solar System with

the detectors of the International Solar Polar mission Ulysses and from radarstudies of meteoroids. The sizes of these particles are about 0.8 �m and 15–30 �m, respectively. They are somewhat larger than typical interstellar grains.

2.6.3Ices

Spectral signatures of ices have been seen in OH/IR stars and other evolved stellarsystems, in lines of sight towards field stars located behind molecular clouds, andaround embedded protostellar objects. More than 20 ice features have beendetected in the IR. Ices create mantles on dust grains. These mantles are importantfor the formation of molecules.H2O ice was detected by Gillett and Forrest in 1973 from the 3-�mwaterline. It is

the most dominant solid-state species, and abundances of other ices are usuallygiven in reference to H2O ice. In clouds with substantial extinction, it is compa-rable in amount or even more abundant than gaseous CO. H2O ice is usually thesecond most abundant molecular species after H2 ([H2O]/[H2] ~ 10–4–10–5). About15–20% of the cosmic H2O is locked in ices, and the remainder is in gas phase.CO2 ice is difficult to detect with ground-based telescopes because of atmos-

pheric CO2. Its firm detection was not established until the late 1990 s with theInfrared Space Observatory (ISO) mission. At present it appears that CO2 is thesecond most abundant ice after H2O ice, with the CO2:H2O ratio being on averageabout 15–20% .CO has been detected in icy form. Although it may conform 3–20% of the ice

component in the grain mantles, it is much more abundant in the gaseous phasethan in the solid phase.CH4 has spectral signatures that are difficult to observe from the ground. The

abundance of CH4 ices is typically 1–2% of water ice. The ratio of gaseous to solidstate is usually below unity, suggesting that CH4 is formed directly by hydro-genation of carbon on the surface of the grain.Formaldehyde (H2CO), the simplest of the hydroxyl group of ices, was detected

from ISO observations towards five massive protostellar envelopes with the typicalabundance of 1–2% to water ice.Methanol (CH3OH) is one of the key elements in interstellar ices, amounting to

up to 10% of water ice content. The formation of methanol ice is still debated. It

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could be caused by hydrogenation of CO or by energetic processes followed byselective desorption enhancement effects.Sulfur-containing ices have been searched for, and only OCS has been detected

so far, with a very low abundance of about 0.1% to water ice. H2S has an upperlimit of 1% for the abundance.N2 and NH3 ices have been searched for, but they have not been reliably detected.

The difficulty with N2 is that the possible signal is extremely weak; in the case ofNH3, the difficulty is separation from other spectral lines.O2 and N2 are IR-inactive molecules, and the upper limits for O2 ice are quite

high: <6% of water ice. No detection of O3 or CO3 has been made, suggesting thatO2 is indeed quite rare. It has not even been found in gaseous form, suggesting thatthe lack of O2 is real and is caused by its high reactivity.Other ices that have been found include OCN– and NH4

+ at a maximum level of afew percent. Tentative identifications include HCOO–, CH3CHO, HCONH2, and(NH2)2CO.

2.6.4Molecules in the Gas Phase

2.6.4.1 Observed PropertiesThe gas phase of interstellar clouds consists of H and He, with H2 being the mostabundant molecule in dense clouds. The second most abundant molecule is CO.O2 and N2 have not been found in the ISM. The upper limit for the abundance ofgaseous O2 towards the dense cores of molecular clouds, deduced from observa-tions of the Submillimeter Wave Astronomical Satellite (SWAS), is [O2]/[CO] < 10–7.Radio observations from the sub-millimeter to centimeter wavelengths have

recovered signatures of about 130 different molecules. One-quarter of these donot contain C, three-quarters do contain C, and out of these, two-thirds containboth C and H (Table 2.2). Astronomers would call about 100 molecules “organic,”whereas organic chemists would give this name to only about 65 moleculesdetected in interstellar space. For astrobiology, the most relevant molecules foundare water (H2O), formaldehyde (H2CO), hydrogen cyanide (HCN), sugars suchas glycoaldehyde (CH2OHCHO), and aliphatic hydrocarbon chains up toH(C�C)5CN.Finding longer molecules is in principle possible, but it becomes more difficult

with each added atom. One reason for this is that the more complex the moleculeis, the rarer it becomes. Another reason is that more complex molecules also havemuch more complex spectra, and their unequivocal identification becomes moredifficult. This has been the case in several claims of the detection of the simplestamino acid, glycine. Some of these have appeared quite convincing. The thirdproblem with complex molecules is that one needs a reference microwave labo-ratory spectrum for each molecule, and they are not trivial to measure. Manyspectral lines in the microwave region still remain unidentified.

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Table 2.2 Interstellar molecules.

Numberof atoms

per moleculeMolecule

2 IF, AlCl, C2, CH, CH+, CN, CO, CO+, CP, CS, CSi, HCl, H2, KCl, NH, NO, NS,NaCl, OH, PN, SO, SO+, SiN, SiO, SiS, HF, SH, FeO(?)

3 C3, C2H, C2O, C2S, CH2, HCN, HCO, HCO+, HCS+, HOC+, H2O, H2S, HNC,HNO,MgCN,MgNC, N2H+, N2O, NaCN, OCS, SO2, c-SiC2, CO2, NH2, H3

+, AlNC4 c-C3H, l-C3H, C3N, C3O, C3S, C2H2, CH2D+(?), HCCN, HCNH+, HNCO, HNCS,

HOCO+, H2CO, H2CN, H2CS, H3O+, NH3, SiC3

5 C5, C4H, C4Si, l-C3H2, c-C3H2, CH2CN, CH4, HC3N, HC2NC, HCOOH, H2CHN,H2C2O, H2NCN, HNC3, SiH4, H2COH+

6 C5H, C5O, C2H4, CH3CN, CH3NC, CH3OH, CH3SH, HC3NH+, HC2CHO,HCONH2, l-H2C4, C5N

7 C6H, CH2CHCN, CH3C2H, HC5N, HCOCH3, NH2CH3, c-C2H4O, CH2CHOH8 CH3C3N, HCOOCH3, CH3COOH, C7H, H2C6, CH2OHCHO, CH2CHCHO9 CH3C4H, CH3CH2CN, (CH3)2O, CH3CH2OH, HC7N, C8H10 CH3C5N (?), (CH3)2CO, NH2CH2COOH(?), CH3CH2CHO11 HC9N13 HC11N

Source: From Al Wootten with permission.

2.6.4.2 Formation of H2

H2 is the most abundant molecule in the Universe, yet it is a difficult molecule toobserve. All the observations have to be made from space-based observatories. In1970, the Copernicus satellite observed H2 electronic lines in absorption against UVbright stars. The ISO operating at IR changed the level of knowledge. Rotationallyvibrated lines from 2–18 �m could be observed. Combining this with informationof other gas-phase atoms, molecular lines, PAHs, silicates, and ices put H2 intoperspective with the other constituents of the ISM.There is no known efficient gas-phase formation mechanism for H2 at low

temperatures and at the densities of the ISM. It is believed that H2 is formed ondust particles, but the detailed formation mechanisms are not known because ofthe limited amount of knowledge about dust particles.To account for the observed amounts of H2, very effective means for its produc-

tion at low temperatures (<30 K) are needed. Models exist whereby H2 is formed onsurfaces of PAHs or on surfaces of very small grains. Several scientists have arguedthat the surface roughness of particles plays an important role.The formation of molecules more complex than H2 has also been studied. The

mechanisms include various combinations of molecule building in the gaseousphase or on grain surfaces, sometimes with the aid of UV radiation, which, bycharging grain surface, can enhance molecule formation.

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2.6.4.3 Formation of CO and H2OAfter H and He, the most common elements in the Universe are O and C. Both COand H2O form readily in gaseous form, possibly in the strong stellar winds duringthe giant phase of stellar evolution. The reservoir of atomic C, which is smallerthan that of O, is nearly depleted in forming CO.The reactions in forming H2O from H and O are among the most exothermic

ones. H or H2 become ionized and react to form H3+. This reacts with atomic O to

form HO+ and H2 as well as H2O+ and H. The ions HO+ and H2O+ react with freeelectrons to form H2O and OH radicals. Thermally, the water molecule is stableuntil a temperature of 3 000 K. This is an important aspect in considering theorigin of Earth’s oceans. H2O can also form directly on grain surfaces.

2.7Generation of Stars: Formation of the Sun and Planets

The formation of a stellar system starts with the collapse of a local dense part of aGMC, the same regions where the most complicated molecules are found. First thedensity increases and central parts of the condensation heat up. The condensation,which is still starless, acquires a higher angular velocity in the center of the densityenhancement. The collapsing system settles into a disk-like geometry. Both thehigher angular velocity at the center and the settling into a disk are due to theconservation of angular momentum. Such dusty disks are seen, for example, in theOrion Molecular Cloud (OMC). They are so dense that even IR does not penetratethrough them, as they appear as dark ellipses of circles against a brighter IRbackground.Some of these “propylads” have a bright star in the center. They have entered an

evolutionary phase at which the condensation in the center has reached a highenough temperature and density that it has turned into a new star. As the starbegins to shine, it will start to ionize H gas around it and a HII region will form. Ifthe newly born stars are located at the edge of the cloud, as inM42, one can note thetypical emission line spectrum, as the tenuous gas emits at a few characteristicwavelengths only. From the spectra one can calculate, among other things, thetemperature and the density of the gas in these HII regions.

2.7.1Accretion Disk of the Sun

When the first generation of normal stars was produced, the building blocks forplanets were not readily available. As we will see later, we need ices and rocks toform planets.It is important to note that the heavier elements C, N, O, Si, and Fe, which are

needed for the planetary building blocks, were produced by nuclear fusions in thefirst generation of normal stars and further processed by the subsequent molecularevolution in the ISM.

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Our Sun and its accretion disk formed in a molecular cloud that was enriched byheavier elements from the first generation of normal stars. Traces of the cloudfrom which our Solar System was formed can be found in meteoritic dust in ourSolar System, e.g., in the form of Al2O3, diamonds, graphite, and SiC within the“fine-grained” matrix in the most pristine chondrite class meteorites.The material that would finally form the stars and planets formed a disk similar

to the ones seen in the OMC. This disk initially consisted of H and He, but all otherelements were also present, as were molecules similar to the ones observed at radiowavelengths in molecular clouds. All the matter began falling towards the centralplane of the disk. The dust grains, both ice-coated and iceless, sedimented to acommon central plane that was to become the general plane of orbits and equatorsof the planets and the Sun. The time it took for the embryonic Solar System toachieve that phase was about one million years.How the planets formed goes along the following line of thought: small dust

particles started to stick together and they grew fairly rapidly into meter-sizeaggregates. Because the aggregates were on similar orbits, their relative velocitieswere small and thus collisions occurred at low-velocity differences. These aggre-gates grew to larger sizes, and once they reached about 1 km, gravitation startedcompacting them. In a few ten thousand years the 1-km particles grew into1000-km planetesimals. At this point they were already so large that the gravitystarted to act on their shape making them round.The speed of the planet formation processes following next can be estimated by

observing dusty disks around solar-type stars of different ages and by correlatingthe age of the star with the state of the disk. For a solar-type star, a planet-formingdisk, the protoplanetary disk, disappears in about 7 million years. After that time,no substantial amount of gas and dust is available for planet formation, althoughdebris disks can last for 400 million years. Somematter remains even for billions ofyears (e.g., zodiacal light and Kuiper Belt objects). Modeling of disks gives similartimescales.Models can provide a temperature profile of the disk. The general temperature

profiles are dependent on the distance from the central star, usually r–0.75 to r–1. Innormal air pressure, H2O would crystallize into ice at 273 K. In space, where H2Osublimates from the solid phase directly into the gas phase, the sublimation pointcan be as low as about 150 K. Beyond some distance from the star, at the so-calledsnow line, H2O ice stays in a solid phase. Inside the snow line, H2O ice sublimatesinto the gas phase. One experimental way to estimate this distance is to study thecrystallization temperatures of meteorites, as done by Chris McKay. The separationof ordinary chondrites and carbonaceous chondrites took place at temperatures of450 K. If the carbonaceous chondrites are identified with the C asteroids and theordinary chondrites with the S asteroids, then one can place a rough distance forthe temperature of 450 K at 2.6 AU. This would now set the snow line at some-where between about 5 AU and 15 AU. The inner parts of the disk were hot,implying that ices melted and evaporated. The temperature estimate for theaccretion disk at 1 AU distance from the above models would be about 500–1200 K. Clearly, at these temperatures the newly formed Earth was hot, with no

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water or other volatiles and no atmosphere at the beginning, and was indeed a veryinhospitable place for life. Some protoplanetary disk models suggest a flattertemperature profile and a snow line closer to the Sun, but in general, there isreasonable agreement that the snow line was at about 5 AU.In the inner part of the Solar System, rocky planets were formed. The last

impacts in the planetary accretion were often from nearly similar-size objectsand were quite severe for the final planet. Examples are the Moon-forming impacton Earth, the impact that possibly caused the retrograde spin of Venus, and themantle-destroying impact on Mercury.In the outer parts of the Solar System, beyond the snow line, different processes

took place. There was more solid material around in the form of (mainly H2O) ice.Once the core of Jupiter had grown to about 20 Earth masses, its gravitationbecame large enough even to hold H and He after capturing them. A runawayaccretion took place, whereby Jupiter started to grow rapidly. With its increasedsphere of influence, it grew even larger until all the available matter in its vicinitywas consumed. A similar process also took place with Saturn, Uranus, andNeptune. Beyond the orbit of Neptune, a large number of icy objects were left.These are now known as Kuiper Belt objects. Several 1000-km objects have beendetected in the last 10 years, some of them of the larger than the dwarf planet Pluto.The large gravitational fields of the outer planets affected the dynamics of the

remaining boulders, both the icy ones, the comets, and the iceless ones, theasteroids. Some of these were ejected from the Solar System and others wereslingshot into the inner parts of the Solar System. This had two effects. First,comets and asteroids were cleared from the vicinity of the giant planets, andsecond, the inner planets experienced a shorter, more intensive heavy bombard-ment of asteroids and comets. Comets and asteroids were important in deliveringthe ingredients necessary for life (see Chapter 3).

2.7.2Formation of the Earth

When did the Earth form? Relative abundances of isotopes of various elements inpristine chondrites can be used to determine the age of our Solar System. Thisgives an age of 4.567 € 0.002 billion years, which defines the moment when thetemperature of the chondrites cooled enough for the minerals to crystallize. Theaccretion continued for the next 100 million years. The size of large impactsincreased until the last one, which stripped the protoatmosphere and possiblymelted the whole Earth. This took place about 4.45 billion years ago, as measuredby xenon isotope ratios of the atmosphere. The Moon-forming impact was earlier,possibly some 4.52 billion years ago. It was thought to be a grazing impact ofa Mars-size body. Because of the impact, both bodies melted and the coresmerged to form the core of the Earth. Part of the debris that was ejected intospace appears to have formed the Moon. The first landmasses formed quite earlyon Earth. Zircon crystals collected from the Jack Hills region in western Australiaindicate that granitic crust formed as early as 4.42 billion years ago. One can

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consider that the formation of the Earth ended at this time, although evenpresently the mass of Earth increases by about 20 000 tons per year due to thefall of micrometerorites.At the beginning, the Earth was so hot that its surface was covered by molten

magma, which means a magma ocean (liquid rock!). The acquired atmosphere wassaturated and contained hot H2O vapor, N2, and most likely CO2 and H2. Atpresent, this is our best guess for the atmospheric composition. It is doubtfulthat any measurements will be able to determine the exact constituents of theearliest atmosphere. Note that the Earth experienced a strong greenhouse effect ofabout 2 000 K because of high amounts of both CO2 and especially H2O. The totalpressure of the atmosphere at the surface was about 1000 times the present value.H2 was such a light molecule that Earth was not able to hold it for a long time. TheEarth started to cool by IR radiation. Once the atmosphere cooled to the dew pointof about 200 �C, a long rain began. Most of the H2O vapor in the atmosphere rained.The oceans had formed. The water was still hot, the water was fresh, and themantle below the sea was also hot. The Earth was left with a CO2 and N2

atmosphere.Volcanic activity was high, and volcano islands formed. The hot magma miner-

als, such as peridotite, interacted with water and formed minerals containingcrystal water, e.g., serpentinite. These mineral formations grew larger. They gainedweight and collapsed, sinking into the mantle. These hydrated minerals experi-enced a partial melting at relatively low pressures and temperatures, formingtonalities among others. They were now lighter than the basaltic seafloor andstarted “floating” on it, eventually becoming the main ingredient for continents. Asrocks started to protrude from the ocean, erosion set in. Under high temperatureand high CO2 partial pressure, erosion was enormous, with an estimated rate ofabout one million times the present value. The CO2 dissolved into water, creatingcarbonic acid H2CO3. This reacted with wollastonite (CaSiO3), changing it intocarbonates (CaCO3) and quartz (SiO2). The carbonates sedimented onto the oceanfloor. This was an effective means for removing CO2 from the atmosphere.

2.7.3Early Rain of Meteorites, Comets, Asteroids, and Prebiotic Molecules

The scars of the heavy bombardment of the inner planets by asteroids and cometscan be seen on the “face” of the full Moon. The maria are lava-filled impact cratersof gigantic proportions. Similar impacts took place on Earth about 23 times moreoften than on the Moon. Some of those impacts had enough energy to evaporatethe oceans.Asteroids and comets still abound. Asteroids can be described as large chunks

(10–1000 km) of rocks made of darker and lighter materials. The brightness of anasteroid depends on the geometric effects of the asteroid’s distance from the Sunand its reflectivity or albedo. The short-term light variations that are seen areusually due to rotation only. Comets are large chunks of a mix of clay, ice, and sand.As they approach the Sun on their elliptical orbits, most of them develop a coma

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and some also a noticeable dust and/or ion tail. In addition to geometric androtational effects, brightness variations due to some kind of activity of volatilematerials, such as H2O, CO, are often observed.Meteorites, which are small pieces of asteroid material surviving the reentry to

Earth, have been critical for understanding asteroids, as they have been historicallythe only means to study these celestial bodies. Radio astronomical spectroscopyopened a new window for cometary molecular studies in the 1970 s, and recentspace missions have provided pictures, onsite measurements, and (still unpub-lished) sample returns from these bodies. The study of these bodies is of theutmost importance for understanding the evolution of the Earth and the delivery ofprebiotic molecules to the Earth and other bodies in our Solar System. One has tobear in mind that although comets and asteroids are quite pristine in manyrespects, most of those bodies have been orbiting our Sun for the last 4.567 billionyears and most likely experienced at least some evolution.While asteroids and comets brought global and local destruction to the early

Earth, they brought at the same time key ingredients for building our present Earthand possibly the critical prebiotic molecules for the origin of life.Asteroids and comets are roughly of the same size. It is thought that the main

cause for the difference between these two groups is the site of their formation.Asteroids formed inside the snow line and comets outside of it. Asteroids shouldhave relatively little H2O, while comets should have a significant portion of solidH2O. The distinction between these two groups is not sharp because there aremany objects that are intermediate in character, but roughly speaking, the classi-fication is valid. Most of the known asteroids are concentrated in orbits betweenMars and Jupiter, while most comets have orbits extending far beyond Neptune.The composition of asteroids has been inferred mainly from studies of meteor-

ites. No onsite measurements exist. Several asteroids have been photographed byflyby space probes, so there is some idea of what they look like and what their colorsand albedos are like. This is of great importance in understanding, for example, themodeling of asteroids based on their brightness variations.Meteorites come in three main types: iron, iron-stony, and stony. Iron meteorites

are nearly solid iron-nickel. Stony meteorites usually contain minerals such asolivine and pyroxene and relatively small amounts of iron. The latter are furtherdivided into chondrites and achondrites. The latter are thought to originate fromthe Moon or Mars (see Chapter 8). About 80% of all recovered meteorites arechondrites. These have small chondrules, which are considered to be the originalmolten material that crystallized during the formation of the meteorites. They arethe oldest rocks in our Solar System. Five percent of chondrites are classified intocarbonaceous chondrites, due to their elemental C.If asteroids are assumed to be made of matter similar to meteorites, then it is

quite clear that asteroids delivered iron and nickel and vast quantities of silicates tothe Earth. C is an important ingredient in many meteorites (up to 4%), as is H2O(20% in meteorites). The asteroid Ceres appears to have 25% H2O by mass, whichis more freshwater than found on Earth. The supply of these raw materials wasmore than sufficient for delivering the quantities found presently in silicates

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(continents) and carbon (biosphere). Also, a significant portion of H2O (oceans)may have arrived through asteroids.The outgassing of volatiles in comets has been studied mainly by radio and IR

spectroscopy. Several dozen molecules have been detected, among them H2O,HCN, H2CO, CH4, which all are important ingredients for the origin of life. Recentobservations from the Stardust return mission to Comet Wild 2 revealed that atleast this comet contains particles from the presolar GMC, from the protosolardisk, and also from later reprocessed matter.The Murchison meteorite fell in Australia in 1969 and was almost immediately

collected. It carries a large number – about 70 – amino acids, as well as nucleotides,sugars, and other organic molecules (see Chapter 3). Hence, the ingredients for lifecan be found in our vicinity in space, and this matter is seen falling even nowadays,as shooting stars. One can easily argue that this would be the easiest means forproviding the young Earth with the seeds for life, maybe not in the form of self-destructing shooting stars but rather in the form of lightly floating micrometeor-ites.Comets also contain N-bearing ices. Because the newly born Earth was free of

volatiles, it seems that comets were the delivery mechanism for N2, the maincomponent of our present atmosphere. The secondmost abundant component, O2,appeared in the atmosphere much later about 2.2 billion years ago, when cyano-bacteria started to produce it – maybe – as a waste product of photosynthesis.

2.7.4D/H Ratio and Oceans

The oceans cover about 70% of the surface of the present Earth. Our planet is oftenreferred to as the “blue planet.” If the whole planet is considered, only 0.04% of themass is in the oceans. Still, the question of oceans is an important one becausewater has played an important role in the origin and evolution of life (seeChapter 1).Asteroids and comets delivered H2O and other volatiles to the young Earth.

These volatiles did not have enough time to evaporate significantly, because theasteroids and comets plunged to the inner Solar System from the vicinity of thesnow line or from far beyond it. Alternatively, it has been suggested that asignificant fraction of the H2O originated from H2O within the accretion disk,but it is not clear how this oxygenation of H could proceed in a relatively hotgaseous disk. However, gaseous H2O formed in the protosolar disk could endure,in principle, temperatures up to 3 500 K in the gas phase. Some geologists havesuggested that H2O was trapped in the minerals that formed the Earth and thatH2O was later outgassed by the hot mantle. One argument that has been raisedagainst the cometary origin of water is the deuterium (D) to H ratio (D/H) of H2O.The standard terrestrial reference in geology for the D/H ratio is the

Vienna Standard Mean Ocean Water (V-SMOW), which has a value ofD/H = (155.76 € 0.05) � 10–6. In interstellar molecular hydrogen, the D/H ratio isabout 15 � 10–6: this is the cosmic D/H ratio. Some cold interstellar molecules,

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however, show a large D/H enrichment, with water having HDO/H2O showing anenrichment of a factor of 20–40 or a D/H of 300–600 � 10–6 and DCN/HCN havingan enrichment of up to a factor of 1000 to the cosmic D/H ratio.The first cometary value wasmeasured by theGiottomission for Comet Halley as

HDO/H2O = (330 € 20) � 10–6. This value was in line with what was seen in waterfrom cold interstellar clouds, suggesting that the water in Comet P/Halley waspresolar.This cometary value created a problem in that the oceanic D/H ratio was too low

by a factor of about 2 to be explained by a cometary origin if Halley represented atypical value for a comet. The concept of a “D/H problem” was created. The nextcomets to be measured for the HDO/H2O ratio were Comet C/1995 O1 Hale-Boppand Hyakutake. The relative abundances measured, (330 € 80) � 10–6 and(280 € 40) � 10–6, respectively, were in line with Comet Halley. The controversybetween cometary HDO and oceanic HDO appeared to grow stronger.One can also turn to other planets in our Solar System. The two giant planets

have low D/H ratios: a value of (16 € 3) � 10–6 for Jupiter and of (18 € 5) � 10–6 forSaturn was measured by IRTF telescope, located on top of Hawaii’s toweringvolcano Mauna Kea. They are both close to the cosmic abundance and in agree-ment with the HDO/H2O ratios of the comets. Uranus and Neptune appear to havea higher value, at about D/H = 60 � 10–6. The Huygens mission (see Chapter 9)measured the D/H ratio for Titan, yielding a fractional abundance of(250 € 50) � 10–6. To complete the known HDO/H2O ratios, Mars has a D/H ratioof (810 € 30) � 10–6 or about 5 SMOW, and Venus has a staggering ratio of(25 € 5) � 10–3or 160 € 32 SMOW. Carbonaceous chondrites show typical valuesof 130–170 � 10–6, close to the SMOW value. On Mars and Venus the loss of lighthydrogen can be understood by its escape into space. Titan’s D/H values are notwell understood yet.As noted, the D/H ratio in the Solar System varies considerably, depending on

whether proper D/H is considered or HDO/H2O is measured. If one considers oneof the two types of measurements only, then the variation remains still large ineach type.With a preconceived presumption that the D/H ratios measured in the three

comets mentioned above, namely, Halley, Hale-Bopp, and Hyakutake, are repre-sentative of the comet population that formed Earth’s oceans, and if the D/H ratiosmeasured in the comets and in the seawater represent the D/H at the time offormation of the oceans, then one has a “D/H problem.” In this scenario, Earth’swater came partially from comets and partially from the water vapor bound tograins in the accretion disk.The story does not end here. The HDO/H2O ratio of the comet C/2004 (Mach-

holz) yielded an upper limit of 230 � 10–6 (3�), obviously below the value from othercomets. HDOwas also detected in comet C/2001 Q4 (NEAT), but no value has beenpublished so far for the D/H ratio. Recent observations of the comet C/1999 S4(LINEAR) suggest that this comet has a very different chemistry than comets suchas Halley, Hyakutake, or Hale-Bopp, which have chemistry consistent with theirformation being beyond the orbit of Neptune. The detailed analysis of the abun-

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dances of molecules in comet C/1999 S4 (LINEAR) by Mumma suggests that thiscomet may have formed in the Jupiter–Saturn region, close to the ice line. In thisregion the D/H ratio could have been significantly lower than in the colder spacebeyond Neptune. The delivery of water from these comets could explain the D/H ofthe terrestrial oceans.Finally, the recent Deep Impact mission to Comet Temple and the Stardust

sample return mission from Comet Wild 2 have raised questions of whether thecomets can undergo substantial evolution during their lifetime and whether thesurface of the comet represents the conditions inside the core.

2.8Further Reading

2.8.1Books or Articles in Books

Despois, D., Biver, N., Bockl�e-Morvan, D.,Crovisier, J. Observations of molecules incomets, in: D. C.Lis, G. A. Blake, E. Herbst(Eds.) Astrochemistry – Recent Successes andCurrent Challenges, IAU Symp 231, pp.19–128, 2005.

Irvine, W.M., Schloerb, F. P., Crovisier, J.,Fegley, B. Jr., Mumma, M. J. Comets: A linkbetween interstellar and nebular chemistryin: V. Mannings, A. P. Boss, S. S. Russell(Eds.) Protostars and Planets IV, University ofArizona Press, pp. 1159–1200, 2000.

Karttunen, H., Krçger, P., Oja, H., Poutanen,M., Donner, K. J. (Eds.), Fundamental As-tronomy, 4th ed., Springer, Berlin, Heidel-berg, New York, 2003 (a good comprehen-sive book for astronomy).

Thomas, P. J., Chyba, Hicks, R. D., C. F.,McKay, C. P. (Eds.) Comets and the Originand Evolution of Life, 2nd ed., Springer, Ber-lin, Heidelberg, New York, 2006.

2.8 Further Reading 51

2.8.2Articles in Journals

Abe, Y. Physical state of the very early Earth,Lithos 1993, 30, 223–235.

Abergel, A., Verstraete, L., Joblin, C., Laureus,R., Miville-DeschÞnes, M-A. The cool inter-stellar medium, Space Sci. Rev. 2005, 119,247–271.

Acharyya, K., Chakrabarti, S. K., Chakrabarti,S. Molecular hydrogen formation duringdense interstellar cloud collapse, Mon. Not.R. Astron. Soc. 2005, 361, 550–558.

Barlow, M. J., Silk, J. H2 recombination oninterstellar grains, Astrophys. J. 1976, 207,131–140.

de Bergh, C. The D/H ratio and the evolutionof water in the terrestrial planets, Origin LifeEvol. Biosphere 1993, 23, 11–21.

Bockel�e-Morvan, D., Gautier, D., Lis, D. C.,Young, K., Keene, J., Phillips, T., Owen,T., Crovisier, J., Goldsmith, P. F., Bergin,E. A., Despois, D., Wotten, A., Deuteriumwater in Comet C/1996 B2 (Hyakutake) andits implications for the origin of comets,Icarus 1998, 133, 147–162.

Ceccarelli, C., Dominik, C., Caux, E., Lefloch,B., Caselli, P. Detection of deuterated waterin a young proto-planetary disks, in:D. C.Lis, G. A. Blake, E. Herbst (Eds.) Astro-chemistry –Recent Successes and CurrentChallenges, IAU Symp 231, 2005 (abstract)

Cernicharo, J., Crovisier, J. Water in space: Thewater world of ISO, Space Sci. Rev. 2005, 119,29–69.

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Charnley, S. B., Rodgers, S. D., Butner, H.M.,Ehrenfreund, P. Astro-ph/0204381 2002(14 pages).

Cuppen, H.M., Herbst, E. Monte Carlo simu-lations of H2 formation on grains of varyingsurface roughness, Mon. Not. R. Astron. Soc.2005, 361, 565–576.

Dartois, E. The ice survey opportunity of ISO,Space Sci. Rev. 2005, 119, 293–310.

Dietrich, M., Wilhelm-Erkens, U. Elementalabundances of high redshift quasars, Astron.Astrophys. 2000, 354, 17–27.

Donahue, T.M. Evolution of water reservoirson Mars from D/H ratios in the atmosphereand crust, Nature 1995, 374, 432–434.

Grinspoon, D.H. Implications of the high D/Hratio for the sources of water in Venus’ at-mosphere, Nature 1993, 363, 428–431.

Habart, E., Walmsley, M., Verstraete, L.,Cazaux, S., Maiolino, R., Cox, P., Boulanger,F., Pineau des ForÞts, G. Molecular Hydro-gen, Space Sci. Rev. 2005, 119, 71–91.

Henning, K. Molecular formation in interstel-lar clouds by gas phase reactions, Astron.Astrophys. Suppl. S. 1981, 44, 405–435.

Hornekaer, L., Baurichter, A., Petrunin, V. V.,Field, D., Luntz, A. C. Importance of surfacemorphology in interstellar H2 formation,Science 2003, 302, 1943–1946.

Jehin, E., Manfroid, J., Hutsem�kers, D., Co-chran, A. L., Arpigny, C., Jackson, W.M.,Rauer, H., Schulz, R., Zucconi, J.-M. DeepImpact: High resolution optical spectro-scopy with the ESO VLT and the KECK Itelescope, Astrophys. J. 2006, 641, L145–L148.

Jones, A. P. Interstellar and circumstellar grainformation and survival, Phil. Trans. R. Soc.,Lond. A. 2001, 359, 1961–1972.

Kashlinksy, A., Ardent, R. G., Mather, J., Mo-seley, S. H. Tracing the first stars with fluc-tuations of the cosmic infrared background,Nature 2005, 438, 45–50 (and comments byR. S. Ellis, same issue p. 39).

Kawakita, H., Watanabe, J., Furusho, R., Fuse,T., Boise, D. C. Nuclear spin temperatureand deuterium-to-hydrogen ration of meth-ane in Comet C/2001 Q4 (NEAT), Astrophys.J. 2005, 623, L49–L52.

Kouchi, A., Greenberg, J. M., Yamamoto, T.,Mukai, T. Extremely low thermal conduc-tivity of amorphous ice: Relevance to cometevolution, Astrophys. J. 1992, 388, L73–L76.

Lecar, M., Podolak, M., Sasselov, D., Chiang, E.On the location of the snow line in a proto-planetary disk, Astrophys. J. 2006, 640, 1115–1118.

Lorenzetti, D. Pre-main sequence stars seen byISO, Space Sci. Rev. 2005, 119, 181–199.

Meier, R., Owen, T. C., Jewitt, D. C., Matthews,H. E., Senay, M., Biver, N., Bockel�e-Mor-van, D., Crovisier, J., Gautier, D. Deuteriumin Comet C/1995 O1 (Hale-Bopp): Detectionof DCN, Science 1998, 279, 1707–1710.

Meier, R., Owen, T. Cometary Deuterium,Space Sci. Rev. 1999, 90, 33–43.

Molster, F., Kemper, C. Crystalline Silicates,Space Sci. Rev. 2005, 119, 3–28.

de Muizon, M. J. Debris Discs around stars:The 2004 Iso Legacy, Space Sci. Rev. 2005,119, 201–214.

M�ller, T. G., �brah�m, P., Crovisier, J. Com-ets, Asteroids and Zodiacal light as seen byISO, Space Sci. Rev. 2005, 119, 141–155.

Mumma,M. J., Dello Russo, N., DiSanti, M. A.,Magee-Sauer, K., Novak, R. E., Brittain, S.,Retting, T., McLean, I.S., Reuter, D. C., Xu,Li-H. Organic Composition of C/1999 S4(LINEAR): A Comet formed near Jupiter?Science 2001, 292, 1334–1339.

Niemann, H. B., Atreya, S. K., Bauer, S. J.,Carignan, G. R., Demick, J. E., Frost, R. L.,Gautier, D., Haberman, J. A., Harpold,D. N., Hunten, D.M., Israel, G., Lunine,J. I., Kasprzak, W. T., Owen, T. C., Paulko-vich, M., Raulin, F., Raaen, E., Way, S. H.The abundances of constituents of Titan’satmosphere from the GCMS instrument onthe Huygens probe, Nature 2005, 438,779–783.

Nisini, B., Kaas, A. A., van Dishoeck, E. F.,Ward-Thompson, D. ISO observations ofpre-stellar cores and young stellar objects,Space Sci. Rev. 2005, 119, 159–179.

Podolak, M., Mekler, Y., Prialnik, D. Is the D/Hratio in the comet equal to the D/H ratio inthe comet nucleus? Icarus 2002, 160, 208–211and comments by Krasnopolsky Icarus 2004,168, 200 and rebuttal by original authors inIcarus 2004, 168, 221–222.

Robert, F. The Origin of water on Earth, Science2001, 293, 1056–1058.

Roberts, H., Herbst, E. The abundance of gas-eous H2O and O2 in cores of dense inter-stellar clouds, Astron. Astrophys. 2002, 395,233–242.

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Safarik, D. J., Mullins, C. B. The nucleationrate of crystalline ice in amorphous solidwater, J. Chem. Phys. 2004, 121, 6003–6010.

Sasselov, D. D., Lecar, M. On the snow line industy protoplanetary disks, Astrophys. J.2000, 528, 995–998.

Schulz, R., Owens, A., Rodriguez-Pascual,P.M., Lumb, D., Erd, C., St�we, J. A. De-tection of water ice grains after the DeepImpact onto Comet 9P/Tempel 1, Astron.Astrophys. 2006, 448, L53–L56.

Speedy, R. J., Debenedetti, P. G., Smith, R. S.,Huang, C., Kay, B. D. The evaporation rate,free energy, and entropy of amorphous waterat 150K, J. Chem. Phys. 1996, 105, 240–244.

Talbi, D., Chandler, G. S., Rohl, A. L. The in-terstellar gas-phase formation of CO2 – As-sisted or not by water molecule, Chem. Phys.2006, 320, 214–228.

Van�sek, V., Van�sek, P. Prediction of Deute-rium Abundance in Comets, Icarus 1985, 61,57–59.

Varnire, P., Blackman, E. G., Frank, A.,Quillen, A. C. Planets rapidly create holes inyoung circumstellar disks,Astrophys. J. 2006,640, 1110–1114.

Zhang, Y. The age and accretion of the Earth,Earth Sci. Rev. 2002, 59, 235–263.

2.9 Questions for Students 53

2.8.3Web Sites

NASA page on stars and galaxies:http://www.nasa.gov/vision/Universe/starsga-

laxies/index.htmlWilkinson Microwave Anisotropy Probe

(WMAP) page, a NASA Explorer missionmeasuring the temperature of the comicbackground radiation:

http://map.gsfc.nasa.gov/European Southern Observatory:http://www.eso.org/Al Wootten’s page – including a list of known

ISM molecules:http://www.cv.nrao.edu/~awootten/Cologne database on molecular spectroscopy:http://www.ph1.uni-koeln.de/vorhersagen/

main.html

UC San Diego page about ISM:http://cassfos02.ucsd.edu/public/tutorial/

ISM.htmlISO telescope:http://sci.esa.int/science-e/www/object/index.

cfm?fobjectid=32721Near Earth Object program:http://neo.jpl.nasa.gov/Dave Jewitt’s Kuiper belt page:http://www.ifa.hawaii.edu/faculty/jewitt/

kb.htmlUC Berkley geology page:http://www.ucmp.berkeley.edu/exhibit/geolo-

gy.html

2.9Questions for Students

Question 2.1Consider the Si atom in the SiO2 molecule in your porcelain coffee cup and the C

atom in the tiny sugar crystal inside your coffee cup, just before you pour your hotcoffee on it. Where were these atoms formed? How did their long way into yourcoffee cup differ from each other?Question 2.2At any given moment, there are about ten 10-meter meteoroids/asteroids in

Earth’s vicinity, at a distance that is smaller than the Moon’s distance from Earth.Assuming a typical velocity of 10 km s–1, make a rough calculation of how long

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should it take for such an object to hit the Earth. What is the energy liberated insuch an impact? Compare it with something sensible. Compare the mass flux fromthis hypothetical impact with the mass flux from micrometeorites.Question 2.3The triple-alpha reaction is a critical step in the formation of C, and thus in the

formation of life. Find other cosmic steps that have turned out to be critical forgetting together all the important ingredients for life on Earth.Question 2.4Interstellar molecules are observed in gaseous and solid phases. What are the

differences between these groups? Which of the differences are real and which aredue to limitations in observing techniques or due to limiting factors caused by theatmosphere?

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3Basic Prebiotic ChemistryHerv� Cottin

This chapter is devoted to the study of prebiotic chemistry. Itfocuses on the abiotic synthesis of key prebiotic compounds –amino acids, purine and pyrimidine bases, and sugars – fromsimple molecules, such as methane (CH4), hydrogen cyanide(HCN), and formaldehyde (H2CO), thereby filling the gap betweenchemistry and biology. In the first section living systems aredismantled into more elemental fragments: organic molecules. Toaddress the origin of life, the next question is how those fragmentscan be synthesized in an abiotic manner. After a short historicalreview, different tracks of prebiotic chemical evolution are ex-plored: an endogenous production of the molecules of life withinearly Earth’s atmosphere or in the depths of primitive oceans, or anexogenous source of prebiotic molecules through space delivery viameteorites and comets. The last section describes chemical path-ways of the synthesis of the building blocks of life.

3.1Key Molecules of Life

Life as we know it is based on a complex chemistry involving highly sophisticatedbiological molecules such as proteins, ribonucleic acids (RNA), or deoxyribonucleicacids (DNA). Such elaborated structures result from a complex chemical evolution,starting with the simplest organic compounds. At some point, at an as yetundefined stage of complexity and organization of matter, an important step ismade and chemistry turns into biology.

3.1 Key Molecules of Life 55

Complete Course in Astrobiology. Edited by Gerda Horneck and Petra RettbergCopyright � 2007 WILEY-VCH Verlag GmbH & Co. KGaA, WeinheimISBN: 978-3-527-40660-9

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3.1.1Dismantling the Robots

In Chapter 1 Andr� Brack compares the premises of an emerging life to parts of“chemical robots,” which make copies of themselves and are capable of evolutionthrough “mistakes” during reproduction. Following this idea, life could be consid-ered as any type of structure (at a molecular or cellular level or any other form) withsome complexity that bears information to make the robot work and that makescopies of itself. From time to time, the copy would not be the exact image of itsoriginal. This modified copy could be either more adapted to the environment thanits original or less adapted, and therefore either more or less favored to survive.Then it would make more copies of its new model with either more or lessefficiency.Whereas it is quite difficult to find a proper general definition of life (see Chapter

1), it is much easier to answer the question “What is life made of?” The answerturns out to be surprisingly simple. If one considers all living systems on Earth,from unicellular systems such as bacteria to multicellular systems such as plantsand animals, they are all built from the same basic components.Each living system is made of at least one cell. A cell can in turn be broken down

into more elemental parts: proteins, RNA, and DNA molecules embedded withinthe membrane of the cell. These biomolecules are made of mainly the followingelements: carbon (C), hydrogen (H), oxygen (O), and nitrogen (N). The membraneis built from long organic amphiphile chains. These chains possess a polar head,which makes them soluble in water (hydrophilic part of the molecule), and anapolar tail, which is insoluble in water (hydrophobic part of the molecule). Suchmolecules are called amphiphiles (amphi = both), because they consist of both ahydrophobic and a hydrophilic part. These amphiphile structures may self-organ-ize into vesicles (Fig. 3.1).Inside the cell, which is surrounded by the membrane, a complex molecular

engine is working (Fig. 3.2). But, from a simplified chemical point of view, theinterior of the cell turns out to be made of mainly proteins and nucleic acids, suchas DNA and RNA. Of course, there is a wide range of proteins that play various key

3 Basic Prebiotic Chemistry56

Fig. 3.1 Long organic amphiphile chains with a polar head thatmakes them soluble in water and a water-insoluble apolar tail(left), which may self-organize into vesicles (right).

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roles in metabolism and an enormous diversity of DNA and RNAmolecules, whichis reflected by the large diversity of living forms on Earth. But this diversity resultsfrom a combination of 28 molecules only. Every known living organism could becompared with a Lego construction with 28 different kinds of bricks: 20 aminoacids to build the proteins, five purine or pyrimidine bases, two sugars, and onephosphate bridge to build DNA and RNA. The following main functions can beattributed to the three families of molecules:

• DNA stores information,• RNA transmits information, and• proteins act as catalysts.

Table 3.1 shows the basic composition of a cell exemplified by the bacteriumEscherichia coli.

3.1 Key Molecules of Life 57

Fig. 3.2 Basic cellular components (DNA, RNA, and proteins)and functions (storage and transfer of information and proteinsynthesis in the ribosomes).

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Table 3.1 Composition of a bacterial cell as exemplified byEscherichia coli.

Component Percentage of totalcellular weight

Molecular mass(g mol–1)[a]

Water 70 18Proteins 15 40 000RNA 6 ~ 106

DNA 1 2.5 � 109

Carbohydrates and precursors[b] 3 150Lipids and precursors[b] 2 750Amino acids and precursors 0.4 120Nucleotides and precursors 0.4 300Others[c] 2 –

a Averaged in a mixtureb Parts of the cell membranec Other small molecules and inorganic ions

3.1.2Proteins and Amino Acids

Proteins are organic compounds built from a succession of amino acids linkedtogether by peptide bonds. Proteins can play different roles: some are of importanceat a structural level in the cells, while others are enzymes that act as catalysts forchemical reactions. Their properties result from their chemical formula and fromtheir spatial conformation (how the amino acid chain organizes itself in space).An amino acid is a molecule that contains both an amino group (-NH2) and a

carboxylic acid (-COOH) function (Fig. 3.3). If the carbon that bears the amino

3 Basic Prebiotic Chemistry58

Fig. 3.3 (a) General formulaof an Æ-amino acid; R repre-sents different side chains; (b)glycine; (c) 3-dimensionalpresentation of an Æ-aminoacid (alanine) with an asym-metric carbon (marked witha star). Note that these mole-cules, which have an identicalmolecular formula, cannot besuperimposed one over theother.

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3.1 Key Molecules of Life 59

Fig. 3.4 The 20 biological amino acids; association of severalamino acids through peptide bonds produces a polypeptide.

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group is the same as the one bearing the carboxylic function, then the amino acid iscalled an Æ-amino acid. If the amino group is linked to a carbon that is one C awayfrom the carbon bearing the carboxylic function, then the amino acid is called a�-amino acid, and so forth.The general structure of an Æ-amino acid is shown in Fig. 3.3 a. R represents a side

chain specific to each amino acid. In only the simplest amino acid, glycine, is the R-group hydrogen (Fig. 3.3 b). For all other Æ-amino acids, R is different from H. Inthat case the central carbon atomhas four different substituents and is then called anasymmetrical carbon. As shown in Fig. 3.3 c, two spatial arrangements (configu-rations) of these substituents are possible, resulting in two different molecules(called enantiomers) that are mirror images of each other. Molecules with anasymmetric or chiral C atom affect the orientation of polarized light when it passesthrough a sample of molecules of one configuration. Configuration 1 shifts theorientation of polarized light to the right (dextrorotary), while configuration 2 wouldshift it to the left (levorotary). These two configurations of amino acids are called L orD (L-compounds rotate the plane of polarized light to the left, D-compounds to theright). A mixture of equal quantities of both configurations is called a racemicmixture. It neutralizes the effect, and polarized light passes unchanged. Thisproperty toward polarized light has no direct effect on life, but the configurationof amino acid (D or L) is extremely important for the spatial orientation (conforma-tion) of long chains of amino acids: the proteins. The properties of proteins aredirectly linked to their conformation, and they have different characteristics if builtfrom L-amino acids, D-amino acids, or a mixture of both (see also Chapter 1).Asmentioned above, in the proteins the amino acids are linked by peptide bonds.

Peptide bond formation is a condensation reaction leading to the polymerization ofamino acids into peptides and proteins with the concomitant elimination of water(Fig. 3.4). Peptides are small, consisting of a few amino acids. Proteins are poly-peptides of greatly divergent length.To build the proteins, life uses a combination of only 20 amino acids (Fig. 3.4), all

of which appear in one enantiomer: the L-form. Why L-enantiomers were selectedover D-enantiomers remains unknown, but this is a property shared by all livingsystems (with a few exceptions in the bacterial domain; see Chapter 5).

3.1.3DNA, RNA, and Their Building Blocks

DNA (deoxyribonucleic acid) and RNA (ribonucleic acid) are long-chained organicmolecules that contain genetic code information (see Chapter 4). From a chemicalpoint of view, in terms of building blocks of life, their composition and structurecan be quite simply explained.The backbone of DNA and RNA is a succession of sugars (deoxyribose for DNA,

ribose for RNA) linked by phosphate bridges (PO42–) (Fig. 3.5). The “letters” of the

genetic code, which are connected to each sugar molecule, are the purine basesadenine (A) and guanine (G) and the pyrimidine bases cytosine (C), thymine (T) (Tin DNA only), and uracil (U) (in RNA only) (Fig. 3.6). The association of the sugar

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with one of the bases is called a nucleoside. If a phosphate is linked to a nucleoside,the resulting structure is called a nucleotide. The polynucleotide is named accord-ing to the sugar in its structure: DNA if the sugar is a deoxyribose, and RNA if thesugar is a ribose.

3.1 Key Molecules of Life 61

Fig. 3.5 Structure of DNA. DNA and RNA are linked chainsof nucleotides, each consisting of a sugar, a phosphate, andone of the five nucleobases (purine bases: adenine and guanine;pyrimidine bases: cytosine and thymine in DNA or cytosine anduracil in RNA)

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3 Basic Prebiotic Chemistry62

Fig. 3.6 Chemical structure of DNA and RNA nucleotides. Thedifference between the two types of molecules is the substitutionof one H (DNA) by OH (RNA) on the sugar and thymine (DNA)by uracil (RNA).

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The genetic code is encrypted in the specific succession of purine and pyrimidinebases. It contains information about which succession of amino acids is to be builtin which proteins (see Chapter 4). This information is transferred to the ribosomes,the “proteins factory,” via RNA (Fig. 3.2). Ribosomes are composed of RNA andproteins.All living systems function according to this very same mechanism. What makes

a mouse different from an elephant or a mushroom is the number and successionof the “letters” in the DNA molecules.DNA and RNA are usually seen as carriers of genetic information. This picture

has changed with the discovery of the self-splicing of certain RNAs. These obser-vations laid the foundation for the concept of catalytic RNA, the ribozymes (seeChapter 4). This catalytic capacity of RNA led to the idea of the RNA world thatmight have preceded life as we know it today: a simplified cellular biochemicalmachinery in which RNA plays all roles that are essential for life; it carries andtransmits information, and it catalyzes the reactions.

3.1.4First “Prebiotic Robot”

For building the first “prebiotic robot,” and then the first living system, thefollowing compounds must be available:

• long organic amphiphile chains for building membranes;• amino acids for building proteins;• phosphate for the backbone of nucleic acids;• purine and pyrimidine bases as “letters” for the genetic code

in DNA and/or RNA; and• sugars for the nucleic acids (ribose in the RNAworld scenario).

These molecules need to be synthesized under prebiotic conditions, either on earlyEarth or in space. Of course, the presence of the building blocks for life is notsufficient to make the first prebiotic robot; however, they are prerequisites in thescenario of the origin of life.

3.2Historical Milestones

The building blocks of life have been discovered and characterized since the early19th century (Table 3.2). In these early times, the question of the abiotic synthesis ofsuch molecules in the test tube seemed far beyond the scope of most of thechemists’ capabilities. Moreover, it was not even considered as a question ofinterest. It was the generally accepted opinion that organicmolecules are the resultof the activity of organized, i.e., living, systems, and are associated with amysterious“vital energy.” In 1827, the Swedish chemist Jçns Jacob Berzelius (Fig. 3.7) wrote,“Art cannot combine the elements of inorganic matter in the manner of living

3.2 Historical Milestones 63

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nature.” (Berzelius also invented the words “polymerization,” “catalysis,” “electro-negative,” and “electropositive” and discovered the elements selenium [Se], silicon[Si], and titanium [Ti]). At that time, there was no way known to synthesize organicmolecules in the laboratory, and no reason to look for such ways.

Table 3.2 Milestones in the discovery and characterization ofimportant biochemical monomers or polymers.

Year Discoverer Monomer/polymer

1810 W.H. Wollatson Cystine[a]

1819 J.L. Proust Leucine[a]

1823 M.E. Chevreul Fatty acids1838 J.J. Berzelius Proteins1869 F. Miescher DNA1882 A. Kossel Guanine1883 A. Kossel and A. Neumann Thymine1886 A. Kossel and A. Neumann Adenine1894 A. Kossel and A. Neumann Cytosine1900 A. Ascoli Uracil1909 P.T. Levene and W. A. Javok Desoxyribose1906–1936 P.T. Levene et al. Ribose, ribonucleotides

Source: Adapted from Miller and Lazcano 2002.a Amino acid

A firm denial to this theory was brought in 1828 by Berzelius’ friend and formerstudent Friedrich Wçhler (Fig. 3.7). This German chemist succeeded in the firstabiotic synthesis of an organic molecule, urea (NH2-CO-NH2), “without the need ofan animal kidney,” as he said at the time, by simple heating of ammonium cyanate(NH4OCN). From then on, a breach was made in the “vital energy” theory, and,slowly, organic chemistry became the chemistry of carbon-based molecules.

3 Basic Prebiotic Chemistry64

Fig. 3.7 Famous chemists of the 19th century. From leftto right: Jçns Jacob Berzelius (1779–1848), Friedrich Wçhler(1800–1882), Adolph Strecker (1822–1871), and AlexandrButlerov (1828–1886).

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Soon after this pioneering finding, the synthesis of other organic compoundswas realized. Regarding the synthesis of molecules of prime interest to the origin oflife, two major achievements shall be pointed out. In 1850, Adolf Strecker (Fig. 3.7)succeeded in the first laboratory synthesis of an amino acid: alanine from amixtureof acetaldehyde (CH3CHO), ammonia (NH3), and hydrogen cyanide (HCN). A fewyears later, in 1861, Alexandr Butlerov (Fig. 3.7) performed the first laboratorysynthesis of sugar mixtures (also known as the formose reaction) from formaldehyde(HCHO) using a strong alkaline catalyst (NaOH) (see Section 3.4.3).Although these discoveries were very interesting, they were not linked to the

origin-of-life problem. Hence, little progress was made in finding a scientificdescription of the origin of life. One had to wait until 1924 for the publication ofthe book Origin of Life by Aleksandr Ivanovich Oparin (1894–1980). Oparin intro-duced the concept of chemical evolution, which could be seen as the roots of theDarwinian tree of evolution. In this concept, life was the result of a succession ofspontaneous chemical reactions that produce increasingly complex chemical struc-tures. In the first edition of his book (1924) he suggested that such chemicalevolution would take place within an oxidizing atmosphere of the primitive Earth(it was the generally accepted view at that time that the early Earth had an oxidizingatmosphere). In the second edition (1938) he changed the early atmosphere to ahighly reducing environment. Similar ideas were simultaneously developed by theEnglish biologist John Haldane, who was the first to mention the concept of a“prebiotic soup” where chemical evolution took place, a term that became quitepopular in the scientific community studying the origins of life.Some paragraphs of Oparin’s book Origin of Life from 1924 show its actuality:

At first we found carbon scattered in the form of separate atoms, inthe red hot stellar atmospheres. We then found it as a componentof hydrocarbons which appeared on the surface of the Earth. …Inthe waters of the primitive ocean these substance formed morecomplex compounds. Proteins and similar substance appeared.…[They]…acquired a more and more complex and improvedstructure and were finally transformed into primary living beings –the forbears of all life on Earth.

He concluded quite optimistically, bearing promises of spectacular breakthroughsin the field within a few years:

We have every reason to believe that sooner or later we shall be ablepractically to demonstrate that life is nothing else but a specialform of existence of matter. The successes scored recently by Sovietbiology hold out the promise that the artificial creation of thesimplest living beings is not only possible, but that it will beachieved in the not too distant future.

Facing the hard reality of facts, he did temper his optimism and wrote as aconclusion of the second edition of his book in 1934:

3.2 Historical Milestones 65

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We are faced with a colossal problem of investigating each separatestage of the evolutionary process as it was sketched here. …The roadahead of us is hard and long but without doubt it leads to theultimate knowledge of the nature of life. The artificial building orsynthesis of living things is a very remote, but not an unattainablegoal along this road.

As elegant as Oparin and Haldane’s ideas appeared to be, they were expressed at atheoretical level only. The experimental confirmation of the theory of chemicalevolution was provided in 1953 by Stanley Miller, a graduate student in thelaboratory of the Nobel Prize laureate Harold Clayton Urey. They conceivedand built an experiment to simulate a putative primitive Earth environment(Fig. 3.8).In this experiment a gaseous mixture of hydrogen (H2), methane (CH4), ammo-

nia (NH3), and water (H2O) was exposed to an electric discharge that simulated thatof storm lightning. The mixture was connected to a bulb filled with liquid waterthat could be heated. This experiment resulted in the production of a large amountof organic molecules, including several amino acids. Those measurements wereexperimental proof of the theory of chemical evolution. They showed that thechemistry between simple molecules, which were abundant in the atmosphere of

3 Basic Prebiotic Chemistry66

Fig. 3.8 Miller–Urey experiment, which simulates in the labora-tory the coupled chemistry between the primitive Earth atmos-phere (upper right bulb) and warm oceans (lower left bulb). Inthe first version, an atmosphere made of CH4, NH3, H2O, and H2

was considered. A spark discharge simulated storm lightning.

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the primitive Earth, led to the synthesis of key compounds that in turn might haveled to the forms of life as we know it on Earth.The choice of a reducing atmosphere with C as CH4 and N as NH3 (Table 3.3)

was motivated by the following considerations:• CH4, NH3, H2O, and H2 had been detected in the atmosphere

of giant planets since the 1930 s.• All the primitive atmospheres of planets were identical, cap-

tured from the Solar Nebula.• Giant planets, cold and distant from the Sun, have kept their

original composition.

Therefore, Urey and Miller concluded that the current composition of the atmos-phere of giant planets of the Solar System was a good proxy for the composition ofthe atmosphere of the primitive Earth.

Table 3.3 Classification of planetary atmospheres, in terms oftheir redox potential, as a function of their composition.

Redox state of the atmosphere Composition

Reducing CH4, NH3, H2O, H2

CO2, N2, H2O, H2

CO2, H2, H2ONeutral CO2/CO, N2, H2OOxidizing CO2/CO, N2, H2O, O2

However, several recent findings disprove this argumentation. First, it is now quitewell established that telluric planets do not have sufficient mass to capture theSolar Nebula gas like the giant planets did. To do this, a minimummass of 10 to 15Earth masses is required. Only then can a forming planet efficiently trap thevolatile elements of the nebula to form its atmosphere. In addition, recent obser-vations have supported the conception that at a distance of one astronomical unit(AU) from the Sun – that is where the Earth accreted – the gaseous component ofthe Solar Nebula was probably dominated by CO2 and N2. Second, Earth, likeVenus and Mars, has a secondary atmosphere built from volatile compounds thatoutgassed from the mantle on one hand or were imported via meteorites andcomets on the other hand. Third, the composition of the primitive Earth atmos-phere was most probably dominated by CO2 and N2, in which organic syntheses arenot as efficient as in a reducing atmosphere (see Section 3.3).Even if the Miller–Urey experiment is not as conclusive as thought at first glance,

it was a great achievement because it showed that important prebiotic compoundscan be abiotically synthesized in environments simulating “natural” conditions. InSection 3.3 different kinds of such “natural” environments are presented that allowan interesting “prebiotic” chemistry.

3.2 Historical Milestones 67

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3 Basic Prebiotic Chemistry68

Table3.4

Organ

icmolecules

synthesizedin

Miller-typeexpe

rimen

tsas

afunction

ofthecompo

sition

ofthestarting

mixture,

afterelectron

impa

ctor

photolysisas

energeticinpu

ts.C

ompo

unds

inthesolid

-pha

seresidu

esareusua

llyde

tected

afteracid

hydrolysis.

Gaseous

mixture

Redox

state

Related

plan

etary

atmosph

ere

Families

ofsynthe

sizedorganicprod

ucts

Electricdischa

rge

Photolysis

CH

4+NH

3+H

2O(+

H2)

Reducing

Giantplan

ets

RH

(saturatedan

dunsaturated)

HCN

andother

nitriles(saturated)

RCO

2HH

2CO,o

ther

aldehydes

Keton

esan

dalcohols

Solid:A

minoacidsan

dnitrogenated

heterocyclesafterhydrolysis

RH

(mostlysaturated)

HCN

RCN

(saturated)

ifN/C

<1RNH

2ifN/C

>1H

2CO,o

ther

aldehydes

Keton

esan

dalcohols

Solid:A

minoacidsafterhydrolysis

CH

4+N

2(+

H2O

)Reducing

Titan

,Triton

RH

(saturatedan

dunsaturated)

HCN

andother

nitriles(saturatedan

dunsaturated)

includingHC3N

andC2N

2

H2C

O,o

ther

aldehydes

Keton

esan

dalcohols

Solid:A

minoacidsan

dnitrogenated

heterocyclesafterhydrolysis

RH

(saturated&unsaturated)

H2C

O&other

aldehydes

withlow

yields

Solid:C

arbo

xylic

acids

CO

+NH

3+H

2OReducing

HCN,o

xygenated

organic

compo

unds

Solid:A

minoacidsafterhydrolysis

HCN,o

xygenated

organiccompo

unds

Solid:A

minoacidsafterhydrolysis

CO

2+N

2+H

2O+CO/H

2Neu

tral

PrimitiveEarth?

RH

(mostlysaturated)

HCN,o

ther

nitriles(saturated)

H2C

O,o

ther

aldehydes,k

eton

esSolid:A

minoacidsafterhydrolysis

RH

(mostlysaturated)

HCN,o

ther

nitriles(saturated)

H2C

O,o

ther

aldehydes,k

eton

esSolid:A

minoacidsafterhydrolysis

CO

2+N

2+H

2ONeu

tral

PrimitiveEarth?

Ven

us,Mars

Nosynthesis

Nosynthesis

Sou

rce:Adapted

from

Rau

lin20

01.

RH

=hydrocarbon

s

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3.3Sources of Prebiotic Organic Molecules

3.3.1Endogenous Sources of Organic Molecules

3.3.1.1 Atmospheric SynthesesMiller and Urey thought that the first building blocks of life were synthesized inEarth’s primitive atmosphere. For the reasons discussed above, the gaseous mix-ture they chose is no longer considered to be representative of Earth’s earlyatmosphere. Table 3.4 shows some results obtained in different “Miller-type”experiments, using different gaseous mixtures and energy sources.Energy inputs through electric discharges represent lightning or electron inputs

in the atmosphere. For example, in the case of Saturn’s moon Titan, electronstrapped in the magnetosphere of Saturn cascade down into Titan’s atmosphere(see Chapter 9). Photolysis experiments simulate the energetic inputs of the Sunvia energetic UV photons that initiate chemical reactions. Using different energysources but the same atmosphere led to minor differences in the resulting prod-ucts.In contrast, a high sensitivity of the resulting syntheses to the starting gaseous

mixture was observed. Reducing gaseous mixtures, such as the one chosen byMiller and Urey, are the most efficient ones in the formation of complex organicstructures. However, current models of the primitive atmosphere of Earth suggesta rather neutral atmosphere, and such environments are not as efficient in initiat-ing chemical evolution as reducing ones. Figure 3.9 shows the yield in amino acids(percentage of initial C) as a function of the composition of the simulated atmos-phere when performing Miller-type experiments. In a reducing atmosphere, ifcarbon is in a reduced state (in the form of CH4), a large diversity of amino acids issynthesized in a rather efficient way. On the other hand, if carbon is in an oxidized

3.3 Sources of Prebiotic Organic Molecules 69

Fig. 3.9 Amino acid yield (percentage of initialC) as a function of the simulated atmospherecomposition in Miller-type experiments,performed at room temperature and in thepresence of liquid water. Results were obtainedafter 2 days of electric discharge experiments.

Partial pressure of N2, CO, or CO2 was 100 Torr(131 hPa). (A) A great diversity of amino acidswas produced. (B, C) Glycine predominated;little else was produced except a small amountof alanine (adapted from Miller and Lazcano2002).

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state (CO or CO2), the amino acid glycine predominates, and the reaction yields aremuch lower than those using CH4. Moreover, in the absence of CH4, the yield ofamino acids drops significantly if the atmosphere is depleted in H2 and becomesmore and more neutral.Therefore, if the Earth mantle was less oxidized 3.8 billion years ago than today,

an important amount of CH4 could have been emitted through volcanism. In thiscase, endogenous Miller-type syntheses are possible. It has been estimated thatdepending on the redox state of the atmosphere, the endogenous production couldvary by several orders of magnitude, leading to a steady-state concentration oforganics in primitive oceans ranging from 0.4 10–3 g L–1 to 0.4 g L–1. However, itmust be stressed that to date the actual amount of reduced gas in Earth’s primitiveatmosphere is not known.

3.3.1.2 Hydrothermal VentsThe synthesis of organic compounds at the bottom of the ocean in hydrothermalvents (also known as black smokers; Fig. 3.10) has to be considered as anotherendogenous source of prebiotic molecules. Where oceanic plates drift apart, sea-water circulating through the ocean crust is heated up, and it dissolves andexchanges chemicals with the rock. At some places it springs back to the oceanfrom black smokers at a high temperature, enriched in gas, ions, and minerals.Catalytic clays and minerals interact with the aqueous reducing environment richin H2, H2S, CO, CO2, and CH4 (and possibly HCN and NH3). When exhaustedfrom the vent, the dramatic drop in temperature, from 350�C to about 2 �C, favorschemical reactions and polymerizations.It has been shown experimentally that amino acids can be synthesized in such

conditions (high temperature and pressure, reduced environment, and rich inminerals, which can act as catalyst). But one has to take into account that moleculessynthesized in the vicinity of black smokers can also be destroyed because of thehigh temperature. Nowadays, a volume equivalent to the world’s entire ocean

3 Basic Prebiotic Chemistry70

Fig. 3.10 Hydrothermal vents (photograph on the left courtesyof NOAA).

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system circulates through hydrothermal vents every 10 million years. Their pres-ence would have fixed an upper limit on the concentration of organics in theprimitive ocean. More experimental data and field measurements are required toassess the feasibility of this mechanism.

3.3.2Exogenous Delivery of Organic Molecules

Remote sensing observations have given evidence that organic chemistry is veryactive in interstellar molecular clouds, as much in the gaseous phase as in the solidphase (interstellar ices) (see Chapter 2). HCN, HC3N, and HCHO have beendetected. Such molecules are of great astrobiological interest, as will be discussedin Section 3.4. Our Solar System is thought to be the result of the collapse of such acloud.Laboratory experiments simulating the conditions in the molecular clouds

predict the existence of molecules that are much more complex than the onesalready detected by remote sensing. These experiments aim to reproduce thechemistry occurring in interstellar ices. For this, gaseous mixtures consisting ofsimple volatile compounds (H2O, CO, CO2, CH4, NH3, CH3OH, H2CO, andothers), which have been detected in interstellar environments, are introducedinto a cryostat. These molecules then condense onto a cold finger where they forman icy mixture. If exposed to irradiations (either photons or charged particles) or tothermal cycles, chemical reactions between these simple compounds, which the iceis made of, lead to the formation of much more elaborated organic structures,which remain solid at room temperature. This refractory residue was called “yellowstuff” by Mayo Greenberg, the astrophysicist who conceived these laboratoryexperiments in the late 1970 s. From those simulations, one can infer that inmolecular clouds a large amount of organic matter should be frozen on condensa-tion nuclei made of silicates (Fig. 3.11).

3.3.2.1 CometsIt is generally accepted that during the formation of our Solar System the originalcomposition of interstellar grains was lost, because they were either incorporatedin the Sun or planets or pyrolyzed in locations close to the Sun. Turbulent radial

3.3 Sources of Prebiotic Organic Molecules 71

Fig. 3.11 Interstellar grain model: silicate core embedded ina mixture of complex refractory molecules, coated with ice ofvolatile compounds.

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mixing in the Solar Nebula can bring interstellar ices to the warmest parts of thenebula where they would sublimate (Fig. 3.12). Inside the turbulent region, radialmixing brings interstellar grains close to the Sun, resulting in a loss of their initialcomposition. According to models, this turbulent region of the Solar Nebula mighthave extended up to the orbit of Neptune (about 30 AU). Beyond this region, grainsmight have remained in a cold environment and thus might have kept an unalteredinterstellar composition. Hence, the extension of the turbulent region determinesthe chances of keeping pristine interstellar matter in small, undifferentiated icybodies: the comets.Cometary models consider that interstellar organic matter undergoes different

levels of transformation before it will be stored in comets. In some models, cometsare considered to be aggregates composed of unaltered interstellar grains. From arather different point of view, comets are considered to be made of mattercompletely reprocessed in the Solar Nebula. Other models consider an intermedi-ate scenario, which is probably the more realistic one.Putting aside the discussion about the origin of cometary matter, observations

show an undeniable abundance of a large variety of organic compounds in comets.Molecules such as HCN, HCHO, or HC3N, which have been detected in severalcomets, might have an origin in the interstellar medium or might have been

3 Basic Prebiotic Chemistry72

Fig. 3.12 Scheme of the evolution of matter in our SolarSystem: from a natal molecular cloud, the Solar Nebula, untilits incorporation into Solar System bodies (Molecular cloudbackground courtesy of NASA, Solar System background cour-tesy of ESA).

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produced inside the Solar Nebula. In either case, they are of the same astro-biological interest.In 1961, John Oro calculated the amount of organic molecules that could have

been delivered to the Earth via comets as follows: if one considers a typicalcometary nucleus with a density of 1 g cm–3, a comet 1 km in diameter wouldcontain about 2 � 1011 moles of HCN. This amount is equivalent to about 40 nmo-les cm–2 of HCN distributed over Earth’s surface. It corresponds to an amountcomparable to the yearly production of HCN by electric discharge in a CH4-richreducing atmosphere.As predicted in laboratory simulation experiments, in situ measurements in

close vicinity to the comets 1P/Halley (in 1986) and 81P/Wild 2 (in 2004) bearwitness to the existence of more-complex structures that – because of their highmolecular mass – remain in the solid phase on dust grains when ejected from thecometary nucleus. It must be stressed that the lack of liquid water in comet nucleiover long periods of time excludes the possibility of the existence of life in or oncomets – even if short periods of ice melting occur after nucleus formation causedby the decay of radioactive elements.Summing up, comets are considered to be exogenous sources of prebiotic

molecules of great astrobiological potential. This has been inferred from measure-ments in space as well as from laboratory simulation experiments. Therefore,comets are the target of several past, current, and future space missions, such asNASA’s Stardust (http://stardust.jpl.nasa.gov/) and Deep Impact missions (http://deepimpact.jpl.nasa.gov/) and ESA’s Rosetta mission (http://rosetta.esa.int/).

3.3.2.2 MeteoritesBy definition, meteorites are celestial bodies that reach the surface of the Earth.Meteorites – more specifically, those belonging to the carbonaceous chondritefamily (the most famous among them are the Murchison, Murray, and Orgueil)– are another exogenous source of organic molecules. Unlike comets, for which nodirect analysis of the nucleus composition has ever been made, a large number ofmeteorites have been studied with the most sensitive laboratory instruments.The current flux of meteorites is estimated to be about 10 tons per year and was

probably higher on the primitive Earth. A great number of organic molecules havebeen detected in meteorites, such as hydrocarbons; alcohols; carboxylic acids;amines; amides; heterocycles including uracil, adenine, and guanine; and morethan 70 amino acids in the Murchison meteorite. Recently, diamino acids havebeen found in the same object. This shows that molecules once synthesized inspace are able to survive a meteorite impact.Enantiomeric excess at the level of a few percent has been measured for some

amino acids in the Murchison and Murray meteorites. This could give us a key tounderstanding the origin of homochirality in living organisms on Earth. Unlikecomets, the parent bodies of meteorites might have gone through periods withliquid water, which might have led to more advanced stages of chemical evolution.It is interesting to note that some organic compounds extracted from carbonaceous

3.3 Sources of Prebiotic Organic Molecules 73

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chondrites would spontaneously organize to form vesicles. They can be consideredas a type of primitive membrane that might have been used by the very firstorganisms.No space mission is currently scheduled to analyze the composition of carbona-

ceous asteroids, which are probably the parent bodies of chondrites. However,projects to explore a carbonaceous asteroid could certainly be planned in the yearsto come, and this will provide important information about the evolutionary stageof those bodies and the origin of their organic components.

3.3.2.3 MicrometeoritesMicrometeorites are another vector for exogenous delivery of organic molecules.With an asteroidal or cometary origin, their current flux is estimated to be about20 000 tons per year. They slowly sediment in the terrestrial atmosphere and thusundergo little warming that could destroy their organic content. Amino acids havebeen detected inmicrometeorites collected in Antarctica. Therefore, they could alsohave played an important role in the origin-of-life process.

3.3.3Relative Contribution of the Different Sources

The three different types of exogenous delivery of organic matter to the early Earth,i.e., by comets, meteorites, or micrometeorites, occurred not only on the Earth butalso throughout the Solar System. However, in order to reach an increased level ofcomplexity that could have led to life, those ingredients require liquid water.Unlike endogenous sources of organics, as inferred by Miller-type experiments

and the hypothesis of black smoker syntheses, which are still at an experimentaland conceptual level, exogenous deliveries are actually observed even nowadays.The contribution of the atmosphere as an endogenous source of organics is stillmodel dependent, and the contribution of hydrothermal vents to produce anddestroy organics lacks experimental data, whereas the exogenous delivery oforganics is an ongoing process.A clear distinction of the relative contribution of each source cannot be estab-

lished and seems to be out of reach as long as no other life forms are detected onanother planet that would be deprived of one or two of these factors. Only thencould it be said that one source is not essential. On the other hand, non-detection oflife on a planet with liquid water and at least one of the three factors could lead tothe conclusion that one specific source of organics is not sufficient for the origin oflife. But from an Earthling point of view, we can say that too many cooks can’t spoilthe prebiotic soup and that the processes leading from the rather simple buildingblocks of life discussed in this section to more elaborated structures are moreinteresting.

3 Basic Prebiotic Chemistry74

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3.4From Simple to Slightly More Complex Compounds

In this section, the chemical pathways to synthesize the building blocks of life in atest tube are described. Some of themechanisms presented here are already familiarto students of chemistry or biology, although they generally are not presented froman astrobiological perspective. Students in other fields should not be afraid of thereactions presented here and should retain that simple mechanisms explain theproduction of most of the molecules considered essential to life.

3.4.1Synthesis of Amino Acids

The synthesis of amino acids has been known since 1850 and was discovered byAdolf Strecker. The mechanism is now well established (Fig. 3.13) and proceeds inliquid water as follows:

• In the first step, the addition of ammonia to aldehyde pro-duces an imine.

• In the second step, the addition of HCN onto the imineproduces an Æ-aminonitrile.

• In the final step, the hydrolysis of the -CN function (nitrile)into -CO2H (carboxylic acid) leads to the production of anamino acid.

In works published after the release of his first results in 1953, Stanley Millershowed that the production of amino acids during his experiments followed the

3.4 From Simple to Slightly More Complex Compounds 75

Fig. 3.13 Synthesis of an amino acid through Strecker synthesis,with H2CO, NH3, and HCN.

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same synthesis processes (see Fig. 3.13). Other pathways are also possible, becauseit has been shown that an acid hydrolysis of HCN polymers results in theproduction of various amino acids.

3.4.2Synthesis of Purine and Pyrimidine Bases

Synthesis of the purine base adenine follows a spectacular prebiotic synthesispathway that proceeds by oligomerization of HCN in aqueous solution underthe influence of photons of 350 nm. This process was discovered by James P.Ferris and Leslie Orgel in 1966 (Fig. 3.14). It proceeds as follows:

• In the first step, the addition of four HCN compounds resultsin the formation of diaminomaleonitrile (DAMN).

• In the second step, a first-photon-step rearrangement ofDAMN results in the formation of diaminofumaronitrile andthen a second one in the formation of aminoimidazole car-bonitrile.

• In the last step, the addition of a fifth HCN molecule leads tothe production of adenine.

It is quite stunning to imagine that one of the most poisonous organic compounds,HCN, reacting with itself may result in the formation of one of the “letters” of thegenetic code, i.e., adenine, which is essential for life. Such are the ways ofchemistry.

3 Basic Prebiotic Chemistry76

Fig. 3.14 Synthesis of adenine from HCN.

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3.4 From Simple to Slightly More Complex Compounds 77

Fig. 3.15 Synthesis of adenine and guanine from HCN and NH3.

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Other pathways leading to the synthesis of purine bases are now known, such asthe ones presented in Fig. 3.15. In this example, a mixture of HCN and NH3 leadsto the production of adenine and guanine.Prebiotic pathways leading to the formation of pyrimidine bases have also been

investigated, such as the ones presented in Fig. 3.16. It is interesting to note thatcyanoacetylene (HC3N), the main reactant of the synthesis, is a compound detectedin the interstellar medium and comets and is also efficiently produced by the actionof spark discharges in CH4/N2 mixtures.The direct reaction of HC3N with cyanate (NCO–) gives quite low yields of

pyrimidine products, or it requires a quite large concentration of cyanate(>0.1 M) for higher yields. In 1995, Robertson and Miller showed that afterhydrolysis and formation of cyanoacetaldehyde, the reaction with urea in anevaporating solution (simulating primitive drying lagoons on Earth) forms anoticeable amount of cytosine.These are only a few illustrations of reactions that lead to the production of

purine and pyrimidine bases in prebiotic conditions. It is quite reasonable tobelieve that not all the pathways have been discovered yet, but the synthesis ofthese important compounds is not yet considered a problem for the chemistsstudying the origin of life.

3.4.3Synthesis of Sugars

Synthesis of the sugars required for the backbone of RNA and DNA molecules ismore difficult than that of the previously discussed compounds. Actually, it is notcomplicated to abiotically produce sugars. Butlerov found a simple way to obtainsugars as early as in 1861. This reaction is now known as the “formose reaction”

3 Basic Prebiotic Chemistry78

Fig. 3.16 Synthesis of cytosine and uracil from cyanoacetylene(HC2CN) and cyanate (NCO–).

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(Fig. 3.17). It requires a concentrated formaldehyde solution and a suitablecatalyst, such as calcium hydroxide Ca(OH)2, calcium carbonate CaCO3, or clayminerals.The formose reaction results in a mixture of many kinds of sugars (more than 40

species), in which ribose is present at only a very low level. Hence, the formosereaction, although highly efficient, leads to an unspecific production of sugars.

3.4 From Simple to Slightly More Complex Compounds 79

Fig. 3.17 Synthesis of sugars through the formose reactionfrom H2CO.

Fig. 3.18 Structure of PNA, a hypothetical information-bearingmolecule based on peptides, and of RNA.

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This makes it less interesting from an astrobiological point of view. Moreover, theformose reaction needs a concentrated solution of formaldehyde, which is not veryrelevant for the conditions of the primitive Earth. However, with the use of a propercatalyst, e.g., the clay mineral kaolin, sugars including ribose can be obtained fromlower concentrations (0.01 M) of formaldehyde.Therefore, in the frame of the RNA world hypothesis (see Chapter 4), the

question of why ribose among other sugars has been selected remains open.Because it is so complicated to find a suitable pathway for the prebiotic selectivesynthesis of ribose and to understand how ribose was selected among other sugars,alternative solutions have been suggested, such as a pre-RNA world. This could bebased, for example, on peptide analogues of nucleic acids, which are called “peptidenucleic acids” (PNAs) (Fig. 3.18), in which the sugar would be replaced by aminoacids. In this scenario, ribose would be incorporated into the structure of life’sinformational molecule at a later stage.

3.4.4Synthesis of Polymers

It has been shown in the previous sections that chemistry is not without solutionsto explain how the building constituents of life could have been synthesizedabiotically. The next step would be to associate the prebiotic elements into complexbiochemical material such as polypeptides (proteins) and polynucleotides (RNAand DNA). Here, prebiotic chemistry faces a further challenge.The linkage of amino acids to peptides is not favored from an energetic point of

view. The free enthalpy for the association of alanine (Ala) with glycine (Gly) is˜G� = 4.13 kcal mol–1. This means that the equilibrium is displaced to left and thedissociation of the di-peptide:

H-Ala-OH + H-Gly-OH H-Ala-Gly-OH + H2O (3.1)

˜G� = 4.13 kcal mol–1

37 �C, pH = 7

Reaction 3.1 shows that peptide bond formation is energetically not favored. Thereaction occurs in water and the equilibrium tends to be displaced to the left,because a water molecule is released during peptide bond formation.A thought experiment might illustrate this point. If one considers starting

peptide bond formation from a molar solution (1 mol L–1) of 20 natural aminoacids, thermodynamics says that a resulting protein of about 100 monomer unitswould have a concentration equal to 10–99 mol L–1. This means that 50 times thevolume of the Earth is required to get at least one protein!Other promising ways of polypeptide formation include catalytic synthesis on

mineral surfaces or evaporation–hydration cycle processes with activated aminoacids, e.g., with compounds, in which the acid function of the amino acid is

>

3 Basic Prebiotic Chemistry80

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replaced by an ester function. However, these pathways are still under investiga-tion.The abiotic production of polynucleotides is even more complicated than that of

polypeptides. The reaction of a purine base with ribose in the solid state at 100 �Cresults in their association into a nucleoside with a yield of about 3%. But in thiscase, the base is not linked to the sugar at its “natural” place (Fig. 3.6). Moreover,nucleoside synthesis with a pyrimidine base has not yet been accomplished.As the next step, the reaction of the nucleoside with a phosphate needs to be

considered. Phosphorus is present in igneous rocks as fluorapatite (Ca5(PO4)3F)and in meteorites as chlorapatite (Ca5(PO4)3Cl). Heating at temperatures above100�C leads to the association of the compounds into a nucleotide, but, again, thelinkage of the phosphate does not occur specifically at the “natural” place. To date,the polymerization of nucleotides from their building blocks has not been achievedunder prebiotic conditions.

3.5Conclusions

In this chapter, the basic building blocks of life on Earth and simple ways tosynthesize them under prebiotic conditions have been discussed. But, having theblocks of life does not give a living system. Jacques Reisse, a Belgian chemistworking on the origin of life, says that at the present stage trying to understand thechemistry of the origin of life is like considering building a cathedral (life) buthaving only a pile of bricks (amino acids, sugars, purine and pyrimidine bases).Getting from the bricks to the cathedral, without a plan, an architect, or anyworkers (for the stones have to spontaneously combine themselves), is the chal-lenge chemists are facing. Even if the road is tricky, many chemists have decided todevote their studies to that complicated task. Year after year new discoveries aremade, but it is difficult to know how long it will take before, somewhere in alaboratory, an organic molecule synthesized under prebiotic conditions will behavelike a “robot,” spontaneously making copies of itself and capable of evolution. Todate, it is not even possible to say if such an achievement will ever be made. Whatdoes it take to turn chemistry into biology? Many tracks have to be investigated, andcrucial breakthroughs may not come from the laboratory studies but rather fromthe observation of other bodies in our Solar System. For example, how far does thechemistry go on Mars, Saturn’s moon Titan, or the Jovian moon Europa? Whatdoes it tell us about the origin of life on Earth? These are a few of the manyfascinating questions that need to be addressed in future studies.

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3.6Further Reading

3.6.1Books or Articles in Books

Cronin, J., Reisse, J. Chirality and the origin ofhomochirality, in: M. Gargaud, B. Barbier,H. Martin, J. Reisse (Eds.) Lectures in Astro-biology, Vol. 1, pp. 473–515, Springer, Berlin,Heidelberg, New York, 2005.

Despois, D., Cottin, H. Comets: Potentialsources of prebiotic molecules for the earlyEarth. In: M. Gargaud, B. Barbier, H. Mar-tin, J. Reisse (Eds.) Lectures in Astrobiology,Vol. 1, pp. 289–352, Springer, Berlin, Hei-delberg, New York, 2005.

Greenberg, J. M. What are comets made of?A model based on interstellar dust, in: L. L.Wilkening (Ed.) Comets, pp. 131–163, Uni-versity of Arizona Press, 1982.

Maturana, H., Varela, F. J. Autopoiesis andCognition: The Realization of the Living,Reidel, Boston, 1980.

Miller, S., Lazcano, A. Formation of the build-ing blocks of life, in J. W. Schopf (Ed.) Life’sOrigin, pp. 78–112, University of CaliforniaPress, 2002.

Oparin, A. I. The Origin of Life, Foreignlanguages publishing house, 1924.

Oparin, A. I. Origin of Life, Dover publication,1938.

Oro, J., Cosmovici, C. B. Comets and life on theprimitive Earth, in: C. B. Cosmovici, S. Bow-yer, D. Werthimer (Eds.) Astronomical andBiochemical Origins and the Search for Life inthe Universe, Proceedings of the 5th Interna-tional Conference on Bioastronomy pp. 97–120,Editrice Compositori, Bologna, 1997.

Raulin, F. Chimie pr�biotique: exp�riences desimulation en laboratoire et “v�rit� terrain,”in: M. Gargaud, D. Despois, J.-P. Parisot(Eds.) L’environnement de la Terre Primitive,pp. 343–360, Presses Universitaires de Bor-deaux, 2001.

Raulin, F., Coll, P., Navarro-Gonzalez, R. Pre-biotic Chemistry: Laboratory Experimentsand Planetary Observations, in: M. Gargaud,B. Barbier, H.Martin, J. Reisse (Eds.) Lecturesin Astrobiology, Vol. 1, pp. 449–471, Springer,Berlin, Heidelberg, New York, 2005.

Schopf, J.W. Life’s Origin, the Beginnings ofBiological Evolution, University of CaliforniaPress, 2002.

3 Basic Prebiotic Chemistry82

3.6.2Articles in Journals

Botta, O., Bada, J. L. Extraterrestrial organiccompounds in meteorites. Surveys in Geo-physics 2002, 23, 411–467.

Cottin, H., Gazeau, M. C., Raulin, F. Cometaryorganic chemistry: a review from observa-tions, numerical and experimental simula-tions. Planet. Space Sci. 1999, 47, 1141–1162.

Ferris, J. P., Hagan j., W. J. HCN and chemicalevolution: The possible role of cyano com-pounds in prebiotic synthesis. Tetrahedron1984, 40, 1093–1120.

Hennet, R. J.-C., Holm, N. G., Engel, M.H.Abiotic synthesis of amino acids under hy-drothermal conditions and the origin of life:

a perpetual phenomenon. Naturwissen-schaften 1992, 79, 361–365.

Miller, S. L. The production of amino acidsunder possible primitive Earth conditions,Science 1953, 117, 528–529.

Pascal, R., Boiteau, L., Commeyras, A. Fromthe prebiotic synthesis of �-amino acids to-wards a primitive translation apparatus forthe synthesis of peptides, Top. Curr. Chem.2005, 259, 69–122.

Shapiro, R. Prebiotic ribose synthesis: a criticalanalysis. Orig. Life Evol. Biosphere 1988, 18,71–85.

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3.7Questions for Students

3.7.1Basic-level Questions

Question 3.1Describe the Miller–Urey experiment. What did we learn from its results? What

are its limitations?Question 3.2What are the main sources of organic compounds that are currently considered

for understanding the first steps of chemical evolution towards the origin of life?Could they be the same on Jupiter’s moon Europa? Why or why not?

3.7.2Advanced-level Questions

Question 3.3Draw a scheme describing an experiment attempting to simulate the chemistry

of interstellar ices.Question 3.4Describe the history of a C atom, from its synthesis in a star to its incorporation

into a living system on an imaginary planet harboring life.Question 3.5Describe the extent to which RNAmolecules could be considered living systems.

3.7 Questions for Students 83

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4From Molecular Evolution to Cellular LifeKirsi Lehto

In this chapter, contemporary cellular life is analyzed in order tosee which components are the most ubiquitous and conserved inall life forms and therefore assumed to be the most original func-tional units of life. Molecular analysis of these structures givessuggestions of how they were involved in early molecular evolutionand what functions they may have provided to the early (pre-cellular) replicators. By going backwards, step by step, one seeswhich inventions had to precede each stage of early evolution:genetically encoded proteins had to exist prior to the establishmentof the Last Universal Common Ancestor (LUCA), and RNA repli-cators, or replicating RNA analogues had to predate geneticallyencoded proteins. Special attention is given to the most conservedcomponents of the present life forms, considered to be relicts of theearly RNA world.

4.1History of Life at Its Beginnings

Our home planet was formed about 4.6 billion years ago. The initial conditions onthe young planet Earth were very harsh. The accretion process had heated theprotoplanet, and the temperature of the young planet was further increased by thegreenhouse phenomena caused by the dense atmosphere formed by H2O and CO2

and by continuing impacts from the colliding comets and meteorites. The initialplanet temperature was hot enough to keep the Earth’s crust in liquid form,forming a magma ocean on the surface. As the planet radiated heat, the temper-ature was reduced; when it came down to about 200 �C, with the prevailing highatmospheric pressure, the water vapor precipitated and rained down to formoceans. The dating obtained from the oldest zircon crystals indicates that liquidwater was present on the planet 4.4 billion years ago. The first Earth crust formed

4.1 History of Life at Its Beginnings 85

Complete Course in Astrobiology. Edited by Gerda Horneck and Petra RettbergCopyright � 2007 WILEY-VCH Verlag GmbH & Co. KGaA, WeinheimISBN: 978-3-527-40660-9

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underneath the water. Because of heavy cometary and asteroid impacts, the con-ditions on Earth remained hot and violent for perhaps 500 million years; this timeis called the Hadean period.Conditions during the Hadean period are difficult to investigate because all the

rocks formed during that era have been thoroughly metamorphosed by the tectonicprocesses of the later times. The oldest still existing sedimentary rocks are locatedat Isua, Greenland, and date back to about 3.8 billion years. These rocks containsmall granules of sedimented carbon, which is specifically enriched in the 12Crather than the heavier 13C isotope. The enrichment of the lighter carbon isotope inthese sediments suggests that the carbon was once bound in biologically producedcompounds (see Chapters 1 and 2). The real biological origin of these carbondeposits has been questioned, but other nearly as old samples containing 12C-enriched carbon and fossilized microbial structures have been detected at two otherlocations: in the 3.5-billion-year-old sediments at Pilbara, western Australia, and atBarberton, South Africa. These findings suggest that life was well established, andapparently widely distributed on the Earth, at this very early stage – or soon afterthe heavy bombardment ended and the planet cooled to temperatures conducivefor life. It is not known at what temperature regimes life started. The mostthermotolerant contemporary life forms are known to propagate in temperaturesup to 113�C (see Chapter 5), but the prebiotic replicating macromolecules, and alsothe earliest cellular structures, may have been rather fragile and sensitive forhydrolytic conditions and most likely were not durable in very high temperatures.Since its early start, life has spread and diversified and now occupies all con-

ceivable ecological niches on the Earth (see Chapter 5). During its spread andaccumulation, life has also modified the environment and has profoundly changedthe conditions on planet Earth, including the chemical composition of the atmos-phere, the oceans, and the Earth’s crust. The long-term geological processes oftectonics, volcanism, weathering and erosion, as well as degrading processescaused by life itself, have completely reshaped and mixed multiple times theconditions that prevailed on the early Earth and have abolished most of thechemical and geochemical traces that were formed at this early time. Therefore,there are not any direct data of the conditions that once allowed or induced theorigin of life. It is even not know in what type of locations on Earth – or, potentially,on nearby planetary bodies – life did start. Thus, trying to trace back the veryearliest stages of this process becomes difficult and speculative.However, different scientific approaches may be used to try to resolve what kind

of conditions and what chemical compounds might have driven the life-producingreactions. Clearly, the origin of life has been a very complex process and needs to bestudied in many different fields of science. Astronomy is needed to resolve how theelements, the Solar System, and the planet Earth were formed in the first place.Geosciences are needed to resolve the conditions on the early Earth and thecomposition of the early atmosphere, the ocean, and the crust. Inorganic andorganic chemistry are needed to resolve how the elements, inorganic minerals, andvolatiles may have reacted to form small organic compounds and more complexorganics such as nucleotides and amino acids, which are the building blocks of life.

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Further on, the quest is to resolve how these organic molecules may polymerizeand, in particular, how these reactions might conceivably have happened in pre-biotic conditions in the absence of genetically encoded enzymes and biochemicalreactions.Present-day life is solely driven by multiple protein-catalyzed (-mediated) bio-

chemical reactions and complex molecular interactions. The fields of biochemistryand bioinformatics study how these enzymes and other proteins now function andhow they have changed over the evolution of life. These studies can identify thegenetic sequences that are the most conserved (i.e., the oldest and most originalones) in different life forms. Of particular interest here are the reactions that stillare catalyzed not by proteins but by different RNA molecules. Such RNA enzymes(or ribozymes) may be derived from the very oldest life forms or from the erapredating the DNA-protein-based life forms.As a central part of the study of life, different fields of biology study the essential

structures and functions of life; how life reacts and adapts in its environment; andhow all functions are mediated, regulated, and coordinated on the cellular andmolecular level. All these integrated efforts are needed to construct an under-standing of what life is, how it has evolved through times, and, maybe, how itstarted in the first place.It may be assumed that the chemical and molecular evolution towards life

proceeded through a long cascade of different stages, initiated by spontaneousreactions between abundant chemical elements, or the chemical constituents oflife: carbon, hydrogen, oxygen, nitrogen, sulfur, and phosphor (C, H, O, N, S, P). Insome high-energy conditions these elements formed reduced carbon and nitrogencompounds, such as hydrogen cyanide (HCN), ammonia (NH3), methane (CH4),and formaldehyde (HCHO). In suitable conditions these small organic molecules,together with water (H2O), reacted to form the building blocks of life: the nucleicacid bases (purines and pyrimidines), sugars and other hydrocarbons, and aminoacids (see Chapter 3 and Section 4.2). These, again via multiple chemical reactionsand interactions (which are not well understood as yet), formed polymers andmore-complex molecules. Some of the polymers gained the chemical potential tocopy themselves or to replicate, which was the first major transition towards theorigin of life. Replication initiated molecular evolution, which led to the inventionof genetically encoded proteins and, eventually, to the appearance of the firstcellular life forms. From then on, the diversification of life into all the species ofthe biosphere has been covered by Darwinian evolution.This chapter aims to trace back this process in order to visualize the different

stages of the progress from early organic molecules to cellular life forms. Instead ofstarting from the very beginning and progressing upwards, the chapter starts fromthe central features of cellular life as they are known now, because it is known forcertain that this is what eventually came out of early evolution (at the time ithappened, evolution was random and not directed – the outcome could be knownonly after it had happened). Then proceeding backwards, step by step, it discusseswhat types of simpler forms could have given rise to each of the new and morecomplex innovations.

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4.2Life as It Is Known

4.2.1The Phylogenetic Tree of Life

Life is characterized by endless complexity. On the visible level one can observe themultitude of genera, species, forms, and individuals, each thriving in their owntypical ecological niches. Cells of higher organisms are differentiated into organsand tissues, which each present their specific form and function even that they allare regulated by the same genome of the same individual. Variation of species andsubspecies in the microbial world is vastly larger than that of the macrospecies. Themicrobial species can be separated into three different domains of life. Single-celledorganisms such as yeasts, ciliates, and flagellates, which do posses a nucleus in theircells, together with all the higher organisms belong in the domain of Eukarya. Thecells that do not posses a nucleus belong to the prokaryotes, which again belong totwo distinct domains, the Bacteria (or by older nomenclature, the Eubacteria) andthe Archaea (older name, the Archaebacteria). These three domains of life (Eukarya,Bacteria, andArchaea) each constitute their own and separate lineages of life and canbe distinguished from each other by multiple genetic and biochemical markers.The three domains of life share a large number of common features that are

ubiquitous to life, or are the same or very similar in all living organisms. It isbelieved that these features were inherited from a common ancestor of all lifeforms, the Last Universal Common Ancestor (LUCA). However, the properties ofLUCA at the time of diversification and the exact sequence of the separation of thethree lines are still unclear. Clearly, the common ancestor has developed through acascade of gradually increasing complexity, and it is not quite clear, which stagewas The Last Common One. As reviewed by Delaye and coworkers (2005), it mighthave been a community of simple precursors of life, the so-called progenotes (seeSection 4.3.2), or even a community of free-living replicating molecules, predatingthe establishment of cellular life. However, recent phylogenetic studies (i.e.,studies of the lineages and relatedness of known organisms through statisticalcomparison of their genetic sequences) by, e.g., the groups of Lazcano andDoolittle, indicate that LUCA was a well-established cell line. The properties ofLUCA will be discussed below.

4.2.2Life is Cellular, Happens in Liquid Water, and Is Based on Genetic Information

From unicellular microorganisms to all higher life forms, all life on Earth iscellular (Fig. 4.1). Prokaryotes are single-celled organisms. The cells are simpleand usually devoid of any internal membrane structures (except for the photo-synthetic cyanobacteria, which possess intensive photosynthetic membranes). Thecells are spherical, ellipsoid, elongated, or rod-shaped (see Chapter 5) and of sizesvarying from 0.1 �m to 600 �m, depending on the species.

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All eukaryote cells have intensive internal structure. Cell organelles include• the nucleus (contains the chromosomes or the genomic

DNA);• mitochondria (energy-producing organelles);• the endoplasmic reticulum (internal membranes),• the Golgi apparatus (membranous vesicles for protein pro-

cessing and transport),• lysosomes and peroxisomes (for containment of degradative

enzymes and wastes); and• chloroplasts (photosynthetic organelles; in plant cells only).

The cells of all eukaryotes are very similar to each other, except that the plant cellshave thick and rigid cell walls and contain numerous chloroplasts (or other types ofplastids). Typical sizes vary from 10 �m to several hundred micrometers, but somelarge cell types occur (of a size up to more than 1 m for some nerve cells).Multicellular organismsmay be conceived as tightly bound colonies of individual

cells. The cells are entities contained within the cell membrane, which separates

4.2 Life as It Is Known 89

Fig. 4.1 All life is cellular. (A) Microscopic view of (unidentified)bacterial cells. (B) Scheme of a eukaryotic cell (animal cell on theleft, and plant cell, with a rigid cell wall, on the right) showing theintensive internal structure.

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the cell from its environment but also allows sophisticated communication withthe environment. The communication includes the intake of water and necessarynutrients, excretion of waste products, receiving of chemical signals via differentreceptor molecules, and sending off signals via secretion of different molecules.Thus, the cells dynamically communicate with their environment. All communi-cation through the membrane is mediated via specific proteinaceous channels andstructures embedded in the membrane, because the membrane itself is a hydro-phobic barrier and therefore impermeable to water-soluble molecules.Inside the cells, life is a chemical process where multiple biochemical reactions

take place in aqueous solution. Water functions as the solvent and carrier for ionicand polar molecules, and also is a reacting component in many reactions. Wateralso serves as the exclusion medium to allow the lipid molecules to assemble andformmembranes, and as the medium that interacts with proteins, helping them tofold into their three-dimensional forms. Therefore, water provides a suitableenvironment for the different cellular reactions and for the assembly of importantcellular structures. It provides turgor (internal pressure) and strength to the cells.Water is such an essential environment and requirement for all the life functionsthat it seems likely that the origin of life had to happen in an aqueous environment(see Chapter 1).Proteins, or gene products, have a multitude of essential roles in the cells. They

form several different structures, such as the cytoskeletons in eukaryotes, com-ponents of cell walls, and the porous structures in cell membranes. They regulatereactions such as gene expression and genome replication, and they function insignal transduction by interacting with different target molecules. Still anotherarea where proteins are essential for life is in the (regulated) catalysis of all thereactions going on inside the cells. Most cellular molecules are both synthesizedand degraded via multi-step reaction pathways – and none of these reactionswould happen, at least at any desired rate, without the assistance of proteinaceousenzymes. Even the energy conversion and -releasing reactions have to be medi-ated via enzymatic catalysis so that they happen in a controlled and regulated

4 From Molecular Evolution to Cellular Life90

Fig. 4.2 Chemical reactionrates in dependence of sub-strate concentration, with andwithout enzyme catalysis. En-zymes speed up reaction ratesvery strongly as compared tonon-catalyzed reactions andmake them happen efficientlyeven at very low substrate con-centrations. The maximum rateof reaction is reached when theenzyme becomes saturatedwith the substrate molecules.

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fashion. The enzymes themselves do not participate in the reactions but associatewith the reacting molecules and hold them in such a conformation that thereaction can proceed. Enzymatic catalysis is capable of raising reaction rates bymany orders of magnitude, from nearly zero to very high, and in practice mostbiological reactions would not happen in physiological conditions without enzymecatalysis (Fig. 4.2).Proteins form the tools and the structures in the cells, and genetic information,

encoded in the genomic deoxyribose nucleic acid (DNA), specifies how these toolsand structures are made. Life depends on the function of the proteins and thus onthe genetic information coding for them. Proteins are composed of long chains ofdifferent amino acids, and the sequence of the amino acids in these chains isdetermined by the genes coding for them. From the DNA, the protein-codingsequences are first copied into ribose nucleic acid (RNA) and from this areconverted into amino acid sequences in peptide chains. RNA is a polymer moleculevery similar to DNA; it is composed of similar nucleotide components, with onlythe small difference of an OH group, rather than H, being connected to the carbonin position 2 (2’) in the pentose sugar ring (thus, the sugar is ribose instead of

4.2 Life as It Is Known 91

Fig. 4.3 Structure of the componentsof genetic material: the nucleic acidbases adenine, guanine, cytosine,thymine, and uracil; the deoxyriboseand ribose sugar molecules; and thephosphate moiety.

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deoxyribose) (Fig. 4.3). However, this OH group is very reactive and, differing fromthe DNA, makes the RNA polymers very fragile, unstable, and short-lived.

4.2.2.1 Genetic InformationThe complexity of life extends strongly to the molecular level, i.e., to the nucleicacid and protein level inside the cells. The genetic information is encoded in thegenomic DNA in the sequence of four different deoxyribonucleotides (or, in short,nucleotides), which are the phosphorylated form of adenosine (A), guanosine (G),cytosine (C), and thymidine (T) nucleosides. In RNA, the uridine nucleoside isused instead of the thymidine nucleoside. The nucleosides themselves are formedof the corresponding bases (adenine, guanine, cytosine, thymine, and uracil); ofthese, A and G bases are purines and C, T, and U bases are pyrimidines (Fig. 4.3).The bases are covalently bound to a deoxyribose (in DNA) or ribose (in RNA) sugarto form nucleosides. These are phosphorylated at the carbon at their 5’ position toform nucleotides, and these again are connected into long chains via phospho-diester bonds between the 5’ and 3’ carbons (these are the carbons in positions 3and 5 in the ribose ring) of the adjacent sugars (Fig. 4.4).The number of nucleotides in the genomes varies largely between different

species. The genomes of the smallest prokaryotes are composed of about 0.5 � 106

nucleotides, while the genome of the bacterium Escherichia coli is composed of4.8 � 106 nucleotides. The smallest eukaryotic genomes are about an order ofmagnitude larger, but the more complex ones are many orders of magnitude largerthan the prokaryote genomes. The genome of wheat, for instance, is composed of

4 From Molecular Evolution to Cellular Life92

Fig. 4.4 Schemes of DNA. (A) The deoxyribonucleotide polymerformed by diester bonds between the 3’ and 5’ carbons ofadjacent nucleotides; (B) the double helix of two DNA strandsshowing the base pairing of the nucleic acid bases.

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about 17 000 � 106 nucleotides, the human genome of 3 400 � 106 nucleotides, andthat of the fruit fly of 97 � 106 nucleotides (Table 4.1). Further, the number of genesvaries a lot, being about 400 in the smallest endosymbiotic bacteria (Buchneraaphidicola) and some hundreds of thousands in the largest genomes.

Table 4.1 Genome size and coding content of different types oforganisms.

Species Domain Genome size(million bp)[a]

No of genes Coding (%)

Mycoplasma genitalium Bacteria 0.58 470 100Escherichia coli Bacteria 4.8 4 288 100Methanococcus jannaschii Archaea 1.7 1 738 100Saccharomyces cerevisiae Eukarya 12 6 144 70Caenorhabditis elegans Eukarya 100 18 266 25Arabidopsis thaliana Eukarya 100 25 498 31Homo sapiens Eukarya 3 400 32 000 28[b]

1.4[c]

Triticum aestivum Eukarya 17 000 60 000 Not determinedAmoeba dubia Eukarya 670 000 Not determined

a Million base pairs = number of nucleotides.b Total.c For proteins.

The very large genomes, e.g., those of wheat or amoebas, have not been sequenced.Therefore, their accurate sizes and gene contents are not known as yet but can beestimated from their physical properties. It is clear that genome sizes are correlatedwith neither the size nor the complexity of the different species. This seemingparadox is explained by the fact that the large eukaryotic genomes contain largeamounts of non-coding DNA. In humans, for instance, only about 1.5% of thegenomic DNA codes for protein products, and only about 28% of it is transcribedinto RNA. A large part of the remaining DNA is composed of highly repetitivesequences, which are often referred to as “junk-DNA.” However, the non-codingDNA is not all insignificant, because some of those sequences have importantfunctions as structural elements of the DNA or have contributed (or may contributein the future) to the evolution of the genome.Although the cellular genomes are very large, they function in very controlled

manner. Among all the multiple genes, and in the middle of the very large non-coding sequences, the functional genes are expressed in a highly coordinatedfashion: the amount, timing, and location of the expression of each gene areaccurately regulated. The gene regulation is mediated mostly by different proteins– but in many cases also by small, non-coding RNAs.Different proteins, RNAs, membranes, and small soluble molecules such as

sugars and salts fill up the cellular contents, up to a level of molecular crowding in

4.2 Life as It Is Known 93

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the interior space. Although the cellular contents are very complex, their centralfunctions are uniform between all different cells and between all species. Partic-ularly, the genetic code itself and its expression mechanism are the same, inprinciple, in all species (Fig. 4.5).

4.2.2.2 The Genetic Code and Its ExpressionThe genetic information is encoded in the nucleotide sequences in groups ofthree adjacent nucleotides, the codons, each corresponding to specific aminoacids (or a stop sign). Although the four nucleotides (A, G, C, and T in DNA;in RNA, T is replaced by U) can be organized into a total of 43 = 64 different tripletcombinations, only 20 different amino acids are utilized and coded for in thecurrent life forms – although some prokaryotes use 22 different amino acids.Thus, the coding system includes some redundancy: several codons code for thesame amino acid (Table 4.2). Each gene is composed of a set of triplet codons. Thecode of each gene (or the open reading frame, ORF) starts at a specific ATG tripletin the DNA and continues until it reaches one of the following triplets: TAG,TAA, or TGA, which do not code for any amino acid. These stop codons mark theend of the gene (Table 4.2). In eukaryotes the genes are often interrupted byintervening sequences (introns) that must be removed from the sequence duringits expression process.

4 From Molecular Evolution to Cellular Life94

Fig. 4.5 Flow chart of the expression of genetic information.

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4.2 Life as It Is Known 95

Table4.2

Thegene

ticcode

,com

posedof

triplets

ofthefour

nucleicacid

basesuracil(U

),cytosine

(C),ad

enine(A),

andgu

anine(G

),an

dtheirinform

ation(aminoacid

orstartor

stop

codo

n).

Firstbase

Cod

onSecond

base

UInform

ation

Cod

onSecond

base

CInform

ation

Cod

onSecond

base

AInform

ation

Cod

onSecond

base

GInform

ation

Thirdbase

U U U U

UUU

UUC

UUA

UUG

Phen

ylalan

ine

Phen

ylalan

ine

Leucine

Leucine

UCU

UCC

UCA

UCG

Serine

Serine

Serine

Serine

UAU

UAC

UAA

UAG

Tyrosine

Tyrosine

Stopcodo

nStopcodo

n

UGU

UGC

UGA

UGG

Cysteine

Cysteine

Stopcodo

nTryptop

han

U C A G

C C C C

CUU

CUC

CUA

CUG

Leucine

Leucine

Leucine

Leucine

CCU

CCC

CCA

CCG

Prolin

eProlin

eProlin

eProlin

e

CAU

CAC

CAA

CAG

Histidine

Histidine

Glutamine

Glutamine

CGU

CGC

CGA

CGG

Arginine

Arginine

Arginine

Arginine

U C A G

A A A A

AUU

AUC

AUA

AUG

Isoleu

cine

Isoleu

cine

Isoleu

cine

Methionine,

startcodo

n

ACU

ACC

ACA

ACG

Threon

ine

Threon

ine

Threon

ine

Threon

ine

AAU

AAC

AAA

AAG

Asparagine

Asparagine

Lysine

Lysine

AGU

AGC

AGA

AGG

Serine

Serine

Serine

Serine

U C A G

G G G G

GUU

GUC

GUA

GUG

Valine

Valine

Valine

Valine

GCU

GCC

GCA

GCG

Alanine

Alanine

Alanine

Alanine

GAU

GAC

GAA

GAG

Asparticacid

Asparticacid

Glutamic

acid

Glutamic

acid

GGU

GGC

GGA

GGG

Glycine

Glycine

Glycine

Glycine

U C A G

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The genetic code is interpreted (or expressed) in a multi-step process (Fig. 4.5) thatconverts the sequence of the nucleotide triplets into a linear sequence of thecorresponding amino acids (Table 4.2). First, the sequence of the target gene iscopied (transcribed) into a messenger RNA (mRNA). The mRNA contains thesame sequence as the corresponding DNA, but in contrast to DNA, the RNApolymer is short-lived and is used only for short-term expression of the code.The mRNA associates with the two subunits of the ribosome, which then movesalong the mRNA and recognizes the triplet code, starting from the first AUG codonon the mRNA (corresponds to the ATG on the DNA). The nucleotide triplets arerecognized by the anticodon triplets of the aminoacylated transfer RNAs (tRNAs),which enter into the ribosome complex and bring in the specific amino acidscorresponding to each triplet codon. The peptide bonds between the adjacentamino acids are formed by the catalytic RNA component of the ribosome (riboso-mal RNA, rRNA). As these amino acids are brought into the reaction complex, theribosome joins them into a long chain or “translates” the nucleotide sequence intoan amino acid sequence (Fig. 4.5). The produced amino acid chain is initially calleda polypeptide, but after it folds into the accurate three-dimensional structure, itbecomes a functional protein.Thus, the components needed for the expression of the genetic code are the

mRNA, the tRNAs and the amino acids, and the ribosomes. The ribosome itself iscomposed of multiple proteins and RNAs (varying from 52 to 79 proteins and fromthree to four RNAs in different species). Each of the steps of the gene expression(transcription, tRNA amino acylation, and the translation itself) requires multipleaccessory proteins for correct function and regulation. This strong protein depend-ency of the whole gene expression process creates a dilemma similar to the one ofthe chicken and egg. Proteins are required for expression of the genetic code as wellas for the maintenance (or replication) of the code, and the code is needed for theexpression of the proteins. Thus, how could the genetic DNA first be generated andreplicated, and how was its expression machinery first established – how did thiscyclic process get started?It is assumed that the storage and expression of the genetic information were the

first hallmarks for life as we know it and that these were the key elements in themolecular evolution that led to the birth of the LUCA. They existed already at thetime of the LUCA, and they required functions such as genome replication,transcription and translation, and pathways for amino acid and nucleotide syn-thesis. These functions are so essential for present life that their origin is thecentral part of the question of the origin of life as a whole.

4.3Last Universal Common Ancestor (LUCA)

The features that occur in all life forms are essential to life. Therefore, they shouldhave been present already in the earliest established cellular life, i.e., in the LUCA.Such conserved features include

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• the enclosure or containment in cell membranes,• the genetic code, and• the translation machinery for the expression of the code

(the ribosomes, tRNAs, and amino acids).

Some enzymes related to RNA and amino acid biosynthesis and degradation and toenergy production and use (cell metabolism) also are common to all cellular life. Afurther curious detail that is fully conserved in all cellular life is the symmetrybreaking, or homochirality, occurring in its central molecules: all the amino acidsused in the cellular proteins are of the same stereoisomer type, which is the left-handed (L)-configuration (see Chapter 2), and the deoxyribose and ribose sugarsused in all the nucleotides are of the right-handed (D)-configuration only, meaningthat the bond between the carbons in positions 4 and 5 points up, not down(Fig. 4.4).

4.3.1Containment in a Cell Membrane

As mentioned earlier, all life on Earth is cellular, which means that it is allcontained within, and separated from its environment by cell membranes. Thiscontainment is important for many reasons. Themolecules synthesized in the cellsdo not escape into the environment, and the concentrations of the intracellularmolecules are maintained at desired levels by regulating their synthesis anddegradation. Molecules from outside are transported in and out in a regulatedmanner, and the cellular molecules interact and function in amutually coordinatedway. Further, because the cell membrane physically connects the genomes withtheir respective gene products, the selection for beneficial products and functionsbecomes targeted to their corresponding coding sequences, i.e., the genes canevolve based on their products. The physical connection also allows the jointmaintenance of different segments of the genomes and allows their coevolutiontowards synergistic functions. All in all, the cell membrane allows all cellularcomponents to function and evolve as one coordinated entity and unit.The excellent utility of present-day membranes is related to their highly

sophisticated properties. Cell membranes are formed of amphiphilic (i.e., oneend is hydrophobic and the other end is hydrophilic) molecules called lipids,which aggregate in water and assemble into bilayers (see Chapter 3). These lipidbilayers are themselves impermeable to water, but they are spanned by severaldifferent proteins that serve as transport channels for water-soluble moleculesand as receptors for external signals and cues. The cells may also adjust theproperties of their membranes by changing their protein components or bychanging the saturation level of lipids according to temperature. Cells continu-ously produce new lipids for the growth of their membranes, and different lipidsare produced to construct membranes for different compartments. Thus, mem-branes in current cells are very dynamic and functional. However, the situationwas quite different at the time prior to the existence of the proteins needed for

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lipid biosynthesis or for membrane transport channels. How could the cells becontained at this stage?It is possible that some type of membrane was formed in the early world by

spontaneous assembly of abiotically formed lipids. It has been shown that differentpolar hydrocarbon derivatives, containing 10 or more carbons in their hydrocarbonchain, are amphiphilic molecules that may assemble into bilayers, and these againmay spontaneously form vesicles in aqueous environments. Such aliphatic (or linear)and aromatic (or circular) hydrocarbons are present, for instance, in the carbonaceouschondrites (see Chapter 3). Hydrocarbon–lipid vesicles might have enclosed theearliest genomes and functioned as compartments for their replication. However,this scenario involves severe problems. Because the hydrophobic lipid membranesseparate the organism from the surroundings, they may prevent access to theirresources, such as useful molecules available in the surrounding. Further, becausethe organism is closed inside a “dead” membrane, it may not be able to expand ordivide or to allow its progeny to accumulate beyond its own original compartment.Several membrane chemists, e.g. the research groups of Deamer, Luisi, and

Szostak, have attempted to resolve the assembly and the functional parameters ofspontaneously assembled membrane vesicles. They have shown that the perme-ability of the bilayer membranes is related to the length of the aliphatic carbonchains: modified hydrocarbons of less than 14 carbons are permeable for smallionic molecules, such as amino acids and phosphates. Actually, lipid membranesformed of carbon chains of less than 10 carbons are too permeable to maintain anyion gradient. The membrane vesicles formed of longer fatty acids, such as oleicacid, are semipermeable: small molecules, such as nucleotides or amino acids, maydiffuse through them while large polymers may not. This property would allowspontaneous uptake of nucleotides into the vesicles and retention of the polymersinside them. This process would increase the osmotic potential inside of thevesicles and cause the growth of the membrane via incorporation of more fattyacids drawn from emptier vesicles or frommicelles. Thus, themere hydrophobicityof fatty acids or of other lipid molecules may have caused the prebiotic assemblyand function of primitive, cell-like structures. Indeed, assembly and growth, andeven division of such lipid vesicles, have been demonstrated in laboratory con-ditions. Likewise, nucleotide and amino acid polymerization inside the vesicle hasbeen induced, simulating the assembly of small, artificial cells.To have an adequate supply of the lipids (or of amphiphilic carbon chains) for

membrane assembly, the LUCA would have needed the pathways to synthesizecarbon chains containing at least 10 carbons. A significant dilemma related to theorigin of the lipid biosynthesis pathways is that in present life two completelydifferent types of lipids are used for cell membranes: the Archaea use isoprenoid-type carbon chains (polyunsaturated hydrocarbons with methyl side chains), andthe Bacteria and Eukarya use fatty acid–type (unbranched) carbon chains. Thesetypes of carbon chains are produced via completely different pathways, and thepathway utilized in Archaea does not even exist in Eukarya or in Bacteria. Thus, it isdifficult to deduce what kind of lipid biosynthesis might have been utilized in theLUCA and how this early membrane synthesis gave rise to two different mem-

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brane compositions. It is possible either that several different lipid biosynthesispathways were established in the LUCA population, or that the cellular membranesynthesis pathways were established after the divergence of the three domains.However, this latter scenario would leave open the question of how, or in what, theLUCA was contained.It has been suggested by some geochemists that prebiotic reactions and early life

would have utilized some other types of compartments, formed of inorganic surfa-ces. W�chtersh�user (2003) has proposed that prebiotic chemistry might haveoccurred on surfaces of clays or minerals where the earliest cells might then haveassembled. These minerals would have catalyzed the reactions and stabilized theforming polymers (see Chapter 1). Martin and Russell (2002), Koonin and Martin(2005), and Brown propose that the porous, chimney-like structures of metal sulfide(mainly FeS) precipitates, formed at the hydrothermal vents at the bottom of theearly ocean, functioned as chemically rich, protective hatcheries that providedcontainment and suitable chemical conditions for the chemical evolution towardslife. The main attractions of these latter ideas are as follows.

• Firstly, those metal sulfide mounts were formed from amultitude of small, interconnected compartments, whichmight have served as containments for chemicals and ascatalytic surfaces for reactions.

• Secondly, the hydrothermal vents produced a continuousflow of warm geothermal fluid, full of several different re-duced chemicals, and it maintained a strong reduction gra-dient between the H+-rich geothermal fluid and (supposedly)alkaline seawater, driving the reduction chemistry of themolecules.

• Thirdly, the hydrothermal vents produced a temperaturegradient, providing convection flows to cycle the macromo-lecules between double-stranded and single stages (discussedin Section 4.6).

The combination of all these factors might have allowed the evolution of complexmolecular communities in the cell-like inorganic compartments, until they wereadequately competent to produce lipids and proteins for cellular membranes andstructures and might escape from the hatchery to self-sustained life in the outsideworld.

4.3.2Genes and Their Expression

One experimental way to study what properties and functions were present in theLUCA is to look at which genes or sequences are still common to all the organismswhose sequences are known today (assumably derived from the common origin).Lazcano and coworkers compared a set of fully sequenced genomes and found 283genes that are highly conserved in all Eukarya genomes, 24 that are highly

4.3 Last Universal Common Ancestor (LUCA) 99

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conserved in Bacteria, and 145 that are conserved in Archaea. In all domains thesegenes include putative ATPases (for conversion of proton gradients into adenosinetriphosphate [ATP] synthesis and for utilizing the energy of ATP), genes involvedin transcription and translation, as well as RNA helicase and enolase, phosphor-ibosyl pyrophosphate synthase, and thioredoxin genes, which are involved innucleotide biosynthesis and RNA degradation. Such genes, if they were presentin the LUCA, indicate that the organism possessed means for maintaining itsgenetic information (at least in RNA form) and a translation system. Because theATPases locate in the membranes and produce ATP (as energy compound) byutilizing proton gradients formed across the membranes, this indicates that LUCAhad a cell membrane and produced and used energy in the form of ATPmolecules.Another approach to model primitive life is to analyze what would be the

minimal set of genes required by the simplest cells today. Several groups ofbioinformatists have worked on such questions. Gill and coworkers have searchedthe genomes of the smallest existing cells (bacterial and archaeal species, whichlive as endoparasites inside their host cells) for the set of genes that seemmandatory for them all. The living environments of these species are chemicallyvery rich, and the cells may obtain a large part of all their required biochemicalprecursors from their hosts. Therefore, they have lost the corresponding genesfrom their own genomes and have evolved, by reduction, towards ultimately smallgenomes. Comparison of the genomes of such species revealed that they have 206genes in common. All species have additional genes that allow them to survive intheir specific environment (host), but these 206 genes seem to comprise theobligatory set of genetic information required in all these species. Thus, it canbe reasoned that a comparable set of genes is essential for any cellular life, evenwhen living in the most protected and nutrient-rich conditions. Thus, if the LUCAwas a well-established cellular species, sustained in its own (probably chemicallyrich, easy, and protected) environment, it probably had to possess at least thisnumber of gene different functions.As the early organisms evolved to more complex, the initial sequences were

converted via mutation and recombination to code for new functions. The genomesgrew larger by duplicating, recombining, and modifying what they already had:new genes were often produced from previously existing ones, by recombining andmodifying functional protein domains (3-dimensional structures). Recent proteinstructure analysis by Doolittle and coworkers has identified a set of 49 protein-folding domains (or folding super-families) that are present in all analyzed ge-nomes of the three domains of life, suggesting that these protein-folding structureswere already present in the LUCA. Again, these protein structures occur in theproteins related to translation and to metabolic and glycolytic enzymes.So far, it has been reasoned that LUCA was a fairly complex organism. But how

did it diversify into the three domains of life that we know today? The threedomains differ from each other in such ways that their direct descent from oneanother, in a fixed order, is difficult. Each pair of domains shares some featuresthat are lacking from the third domain (Fig. 4.6), so it seems that none of them isdirectly derived from the others.

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Because the deviation of the three domains from the LUCA is difficult to traceback, the question of the order of the establishment of the three domains remainsopen, i.e.:

• whether the prokaryotes differentiated as two branches fromthe LUCA and then formed the eukaryotes later by mutualfusion;

• whether the eukaryotes were derived directly from the LUCAand later gave rise to the prokaryotes (e.g., by plasmid escapeand reduction processes); or

• whether the three domains diverged separately from a mixedLUCA population.

When this question has been addressed by phylogenetic studies, different resultshave been obtained from different genes. For instance, the classical phylogenetictree based on 16S-rRNA sequences, first produced by Woese and coworkers in1990, shows the early deviation of the Bacteria and Archaea domains, with thethermophilic Bacteria and Archaea at the base of the different branches, and thelater deviation of the Eukarya domain from the Archaea (Fig. 4.7A). However, someauthors, e.g., Poole and Forterre, suggest that the phylogenetic analysis may notaccurately resolve the most ancient sequences: after very long (or very fast)evolution, sequences may become so saturated with mutations that they appearas more conserved in the phylogenetic analysis.When different protein gene sequences are analyzed, diverse phylogenetic trees

are produced for the different sequences. This may indicate that the domains havenot evolved as separate lines but rather that the genes have been mixed by stronglateral gene transfer after the separation of the domains.It is now widely discussed (see reviews by Pennisi and Doolittle) that the

intensive lateral gene transfer between species, and even between domains, mayhave mixed the initial lineages so effectively that it may be difficult to trace back anyoriginal sets of genes associated with the early phylogenetic lines. Such lateral genetransfer would have been possible because the newly separated lineages were stillvery simple, similar, flexible (nonspecific), and rudimentary in their functions.Therefore, they might utilize the same novel functions and structures, even if those

4.3 Last Universal Common Ancestor (LUCA) 101

Fig. 4.6 Distribution of some key conservedfeatures among the three domains of life: eachof them is shared by two domains only.

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were transferred across the domain borders. The DNA exchange could have beenmediated via cell fusions or via direct DNA uptake (gene transfer or cellularconjugation) – or via third parties, such as viruses or plasmids (gene transductionor transformation).Particularly in eukaryotes, the uptake of foreign (prokaryotic) DNA may happen

via eating up (endocytosis) of foreign cells. This process is still a distinct function of

4 From Molecular Evolution to Cellular Life102

Fig. 4.7 Phylogenetic lineage of the three domains of lifedetermined by different genetic sequences. (A) 16S ribosomalRNA sequence (adapted from Woese et al. 1990); (B) severaldifferent sequences (adapted from Doolittle 1999).

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some eukaryotic cells. Mitochondria and chloroplasts are well-known examples,indicating that endocytosis of other species has occurred in the history of differenteukaryotes. In these instances the engulfed prokaryotes were maintained intact inthe cytoplasm and established as beneficial endosymbionts, or organelles, of thecells. Considering the strong lateral gene transfer, the tree of life at its earlier stageslooks rather like a bush (Fig. 4.7B).

4.3.3Hypothetical Structure of the LUCA Genome

The dilemma of the differentiation of the three domains relates to the question of thetype and structure of the LUCA genome. It is commonly thought that LUCA shouldhave been similar to the simplest life forms existing today, the prokaryotes. Accord-ingly, it should have been driven by a small, circular DNA genome. However, Pooleand Forterre and their coworkers argue that the circular, supercoiled prokaryoticgenomes with a single origin of replicationmight represent a later adaptation to veryfast and efficient replication strategies.The most primitive DNA genomes may havebeen linear, like the RNA genomes (see Section 4.4), which are thought to havepreceded the DNA genomes. One argument supporting the idea that the eukaryote-like linear genome structure is themost original one is that specific catalytic RNAs –apparent relicts of the earlier RNA genomes – are still used to process different RNAproducts in the eukaryotes (Table 4.3), while many of them have been replaced bymore efficient (and advanced) protein catalysts in the prokaryotes. Likewise, tRNA-like components are still utilized in the enzymes (telomerases) that maintain thetermini (telomeres) of the linear eukaryote chromosomes, suggesting that theseterminal structures are derived from the genomes of RNA-based life.The primitive RNA genomes may have influenced the ploidy level (the copy

number) and the fragmentation (chromosome number) of the later-arriving DNAgenomes. The early RNA genomes were very fragile and prone to degradation, andthe inaccurate replication processes accumulated multiple mistakes in their se-quences. For these reasons, the genomic components did not grow very large. Inorder to accumulate more coding capacity, the genomes should have been com-posed of multiple short components. To avoid the loss of genetic information dueto high mutation rates, the cells should have maintained more than one copy ofeach genomic component, and thus diploid (or maybe multiploid) rather thanhaploid (prokaryote-like) genomes should have been used (although one has tobear in mind that prokaryotes also normally maintain several copies of theirgenome in each cell). The earlier RNA-genome strategy may have been maintainedafter conversion to the DNA form, suggesting that the earliest cellular genomesshould have been composed of multiple, short, linear components, each presentedin more than a single copy.It is not clear whether the LUCA had evolved, as yet, to the DNA stage, or

whether the transition from RNA to DNA genomes occurred separately in the threedifferent lineages after their separation from the LUCA. Later conversion fromRNA to DNA genomes may be supported by the fact that different types of DNA

4.3 Last Universal Common Ancestor (LUCA) 103

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4 From Molecular Evolution to Cellular Life104

Table4.3

Exam

ples

ofpresen

t-da

yRNAcatalystsan

dotherfunction

alRNAs.

RNA

Function

Distribution

Putative

occurren

cein

theRNA

orRNPworld

Ribosom

alRNAs

Translation:structuralan

dcatalytic

Ubiqu

itou

sYes

mRNAs

Carriersof

thegenetic

code

Ubiqu

itou

sYes

tRNAs

Translation:A

minoacid

tran

sport

Ubiqu

itou

sYes

tRNA

Aminoacid

metabolism

Ubiqu

itou

sYes

tRNA

Replicationprim

erRetrotran

sposon

s,retroviruses,

pararetroviruses

Possibly

Telom

eraseRNA

tRNA-like

prim

erforchromosom

een

dsynthesis

Eukaryotes

Yes

RNaseP

tRNAmaturation

Ubiqu

itou

sYes

snoR

NAs

rRNAprocessing

Eukaryotes,som

eArchaea

Yes

RNaseM

RP

rRNAprocessing

Eukaryotes

Related

toRnaseP

GroupIself-splicingintron

smRNAsplicing

Eukaryotes,som

eProkaryotes

Possibly

GroupII

self-splicingintron

smRNAsplicing

Eukaryotes,som

eProkaryotes

Possibly

srpR

NA

Protein

tran

slocation

Eukaryotes,som

eArchaea

Yes

vaultRNA

Not

know

n–Protein

tran

slocation?

Eukaryotes

Possibly

G8RNA

Maintenan

ceof

ribo

somal

apparatus

atelevated

temperatures

Eukaryotes

Probably

Ham

merheadan

dhairpin

ribo

-zymes

Self-cleavage

andlig

ation

Viroids

andsatRNAs

Probably

Sou

rce:Mod

ifiedfrom

Jeffares

etal.1

998.

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polymerases are utilized by Bacteria and by Archaea and Eukarya. Also, if the RNAgenomes were stabilized via methylation of the 2’ hydroxyl groups of the ribosemolecules, as suggested by Poole, it is conceivable that the RNA genomes mighthave developed to be fairly large, gaining significant coding capacity. Such RNAgenomes may have been adequate to support self-sustained cellular life and toproduce codes for the ribonucleotide reductases, thymidylate synthases, and re-verse transcription enzymes eventually needed to convert the ribonucleotides intodeoxyribonucleotides and RNA sequences into DNA. Forterre suggests that thoseDNA-producing enzymes and, consequently, DNA genomes were invented severaltimes to establish DNA-based viral genomes colonizing the RNA cells and that theywere transferred from those to the RNA-based host cells, in three separate transferevents, to establish the three DNA-based domains of life.Woese has suggested that at the earliest stage of evolution, when the genomes

were still very small and unstable, the fully functional genetic information couldnot exist in individual discrete organisms or genomes. He suggests that these earlygenomes instead formed a diverse community of organisms that dynamicallyinteracted with each other, exchanging, testing, storing, and evolving alternativegenomic sequences. Woese calls these early life forms “progenotes,” which de-scribes the evolutionary stage preceding the fixed genomic life forms, or the“genotes.” Again, it is not clear whether such progenotes would have had a DNAor an RNA genome; maybe they could have been characteristic both before andafter the transition from RNA to DNA genomes.

4.4“Life” in the RNA–Protein World: Issues and Possible Solutions

LUCA appears to have been a fairly complex and well-established organism – butfrom where did this complexity arise? Information flow from DNA into mRNA andthen into proteins (Fig. 4.5) demands multiple functions in between; therefore, it iscommonly thought that the whole genetic machinery had to evolve from a simplersystem. It is supposed that the genetic system preceding the DNA genomes wereRNA genomes, which could have functioned as information storage media and astemplates for translation. It is thought that the protein synthesis became estab-lished at the time of the RNA genomes and that the appearance of the proteincatalysts then allowed the “invention” and establishment of the DNA genomes.Thus, present-day DNA–RNA–protein life would have been preceded by lifecomposed of RNAs and their encoded protein products – or by RNA–protein(RNP) life.At the earliest stages, when the genetic code was translated into protein products,

or the genetically encoded proteins were “invented,” both the codes and theirexpression system were certainly very primitive. The codes had not yet evolved tocode for specific functions, and also the translation system was very inaccurate.Maybe only a few of the currently known amino acids were used. The system wasable to produce only a few short, nearly random polypeptides. The polypeptides had

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not been adapted to specific functions, but maybe some of them could bind to RNAand function as scaffolding or structural proteins, similar to present-day chaper-ones. Such structural proteins may still have been quite useful in stabilizing theRNA genomes and in holding them in suitable three-dimensional structures toenhance their catalytic properties. Such structural proteins probably assisted in themost essential functions of the RNP world, i.e., in the replication of the RNAs. Thehigh mutation rate produced more functional gene products, and in due coursesome proteins appeared that actually catalyzed the replication of RNA genomes.

4.4.1Evolutionary Solutions

The early enzymes were still very inefficient and prone to errors. Therefore, eachtime the genomes were replicated, considerable portions of the nucleotides werecopied wrong and the genetic information was altered. If the sequences mutatedtoo much, it was changed into a non-functional form, the gene was no longermaintained, and the information was totally lost. This critical level of accumulationof errors has been defined by Manfred Eigen as the “error threshold” and is nowknown as the “Eigen limit.” The number of incorrectly copied nucleotides in-creased with the genome length; the longer the genomes, the easier they accumu-lated fatal levels of mistakes. Thus, only fairly short genomes (or genomic compo-nents) could be maintained by this very error-prone replication.Eigen has demonstrated how the evolution of small genomes (e.g., viral ge-

nomes) functions in a cyclic fashion, where repeated improvements of differentsynergistic functions lead to very efficient improvement of fitness and adaptationto new conditions. As described by Poole, this cyclic adaptation and genome-building model seems applicable for the gradual improvement of the RNP organ-isms: the new sequence variants encoded for improved replicase proteins or newcomponents for the translation machinery. These produced better replicase mol-ecules and thereby improved the accuracy of the replication. This again allowed themaintenance of longer genomes – and the increasing coding capacity allowed forthe production of new components for the replication and translation machineries.

4 From Molecular Evolution to Cellular Life106

Fig. 4.8 Darwin–Eigen cycle demonstratingthat Darwinian selection for improved repli-cation and translation allowed maintenanceof larger genomes, and these again allowedfor improved replication and gene expression.Thus, the increasing genome size, new genefunctions, and improving replication andtranslation fidelity have mutually enhancingeffects on the evolution of complexity (adaptedfrom Poole et al. 1999).

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Thus, Darwinian selection for more accurate replication and the correspondingincrease of the genome size (determined by the Eigen limit) together enhanced theevolution towards more complex genomes (Fig. 4.8).

4.4.2Solutions Found in the Viral World

It is of interest that present-day single-stranded (ss) RNA viruses possess multiplefeatures that seem similar to the properties of a hypothetical early RNP organisms.As in the RNP organisms, the viral genomes are composed of short linear RNAsthat code only for a few necessary gene products. The total length of RNA virusgenomes seems to be limited by both the fragility of the RNAs and the Eigen limit(the avoidance of accumulating too many errors by inaccurate replication); thus, atthe present time the longest ss RNA virus genomes – those of the coronaviruses –contain about 30 000 nucleotides. The smallest viral genomes, – those of theleviviruses – are only about 3 500 nucleotides long and code only for three proteins,namely, the replicase protein, the coat protein, and a maturase protein to interactwith the host. These seem to make the minimal protein set required for sustainableviral genomes. In many viruses the replicase proteins are divided in two separatecomponents, the helicase and the replicase, apparently because those proteins needto be produced in very different amounts.The coat protein is required to enclose the RNA and to protect it from degrada-

tion. All viruses encode one or more of other gene products to interact with theirhost cells – mainly in order to suppress the host defense functions – but it appearsthat in principle the replication and the protective functions are the most importantrequirements for viral survival. This may also indicate how important theseproteins may have been to the early RNA replicators.Viruses maximize the use of their limited genomic sequences – they use them in

the most efficient way. They contain a minimal amount of non-coding sequences,and they do not “invest” any coding capacity for producing regulatory proteins,which are so essential for cellular life. Many viruses regulate their essentialfunctions – initiation of replication and translation – by short and simple sequen-ces at the termini of the RNA genomes and by interactions between RNA loops andsequences. With such RNA interactions, some viruses are capable of dedicatingtheir genomic RNAs to function in either the replication or the translation mode,which avoids collision of the two opposite processes.Being parasites of the cellular world, RNA viruses make their living in a chemi-

cally rich environment: the host cells provide all the building blocks of the macro-molecules (the nucleotides and the amino acids) and the translation machinery foruse by the viruses. Likewise, the early RNP organisms had to live in a similarenvironment, because they had no means for synthesizing their own buildingblocks. Through their evolutionary history, the RNA viruses have become veryefficient in their replication and in their adaptation to their own specific hostorganisms. Indeed, in spite of their ultimately minimal size, the RNA viruses arevery successful. There are many more species of viruses than there are cellular

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species, and each cellular species may be infected by several different viral species.It is possible that the (fully evolved) RNP-based life forms were efficient andsuccessful replicators. Apparently they had to be quite advanced in order toproduce adequately large genomic pools to give rise to DNA-based life and cellularorganisms. Some of the early RNP-based replicators may have survived to form thebase for the massive variation of present-day viruses.

4.5“Life” Before the Appearance of the Progenote

4.5.1The Breakthrough Organism and the RNA–Protein World

The first protein-mediated functions initiated evolution towards more and morecomplex biochemistry. Therefore, the initiation of genetically encoded proteinsynthesis has been the key step in the development of any more-advanced life.This event has been considered so essential that Poole and coworkers have namedthe first creature that produced proteins the “breakthrough organism.” But howcould this hypothetical breakthrough organism break through – or, how might ithave come into existence in the first place?Clearly, it had to evolve from simpler systems through a cascade of improving

stages. It was required that it be able to synthesize mRNA-like translatablesequences and to run a primitive translation machinery consisting of ribosomes,tRNAs, and amino acids. Because protein synthesis did not exist prior to this time,the assembly or function of this primitive translation machinery could not havedepended on any specific proteins. Thus, the early translation reactions had to becatalyzed by the existing RNAs alone. This is theoretically feasible because in all thepresent-day life forms, the formation of the peptide bonds between amino acids isspecifically mediated by one RNA component of the ribosomes. Different naturalor in vitro–selected RNA molecules may catalyze many other reactions (for thenatural ribozymes, see Table 4.3). For instance, ribozymes have been found thatcan mediate the amino acylation of tRNAs. Thus, according to experimental data, itmay be postulated that mere RNA components were able to mediate the earliesttranslation process.

4.5.2Primitive Translation Machinery

A logical requirement for the existence of RNA-based translation machinery is thatthis machinery itself was initially generated and maintained in a protein-independ-ent manner. Present-day ribosomes are massive complexes, containing either three(in prokaryotes) or four (in eukaryotes) RNAs that vary in size from 120 to 2 904nucleotides. The genes coding for these RNAs take, together with their interveningsequences, more than 7 500 nucleotides of genomic sequences. It is clear that the

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earliest RNA components were not as long as they are today. As mentioned inSection 4.4.1, the error-prone replication systems produced only fairly short RNAstrands that are estimated not to have exceeded a few hundred nucleotides in length.Thus, it is likely that the proto-ribosome had to be composed of short fragments ofRNA that jointly formed one functional complex. This may still be evident inpresent-day ribosomes, because their interaction with tRNAs may be mimicked bya separate small RNA analogue of the ribosomal RNA sequence and because peptidebond formation is catalyzed by a specific adenine in the core of the ribosomal RNA.Thus, it seems likely that the present-day ribosomal RNAs (rRNAs) developed via acombination of previously existing, small functional subunits.

4.5.3Origin of Ribosomes

Even if the early ribosomes were formed of small separate RNAs, their mainte-nance required that they be reproduced fairly accurately. The mere existence ofsuch a functional complex required that it had evolved gradually from somesimpler structures – which again had been maintained and selected for their

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Fig. 4.9 Model of the early function of the proto-translationmachinery as RNA replication complex (from Poole et al. 1998,with permission from the publisher).

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preexisting function(s). The most important function at this stage would have beenthe maintenance of the existing sequences, namely, the replication of RNAs. Pooleand coworkers have proposed that the original function of the proto-ribosomalcomplex was the replication of RNAs. According to their model, the early proto-ribosomes extended the complementary RNA strand on the RNA template byligating nucleotide triplets (corresponding to present-day anticodon loops) broughtinto the reaction by tRNAmolecules or their primitive precursors. This means thatearly replication was mediated by ligation rather than by polymerization. Incorpo-ration of nucleotide triplets rather than single nucleotides had the advantage ofallowing higher affinity and longer-lasting annealing of the incoming nucleotidesto the template. This allowed more time for the very slow RNA catalyst to performthe ligation (Fig. 4.9).According to this model, it is conceivable that amino acid acylation of the incom-

ing tRNAs was a significant step in the early replication process. The covalentbinding of the amino acids to the -CCA terminus of the tRNAs might have chargedthese molecules with energy, which might have been released by the detachment ofthe amino acid during the polymerization. This process might have been used todrive the polymerization. On the other hand, it is conceivable that the positivelycharged amino acids allowed the proper confirmation (tight folding) of the primitive(negatively charged) tRNAs and/or allowed their binding to the replicase complex.Release of the amino acids from the tRNAs might then have caused a conforma-tional change allowing for the release of the used tRNA from the complex.In any of these scenarios, the interaction between template RNA, ribosome, the

“triplet-reading” anticodons of the tRNAs, and the amino acids would have alreadybeen established at the early RNA replication function, prior to the invention ofprotein synthesis. Peptide bond formation might have been initiated as a sponta-neous reaction between the amino acids brought to close proximity by the incom-ing tRNAs. However, later conversion of the whole replication machinery into atranslation function is difficult to conceive – many things would be have beenrequired to change. For example, the hypothetic cleavage and ligation of thenucleotide triplets from the tRNAs and into the growing chain of RNA neededto be stopped and replaced by peptide bond formation. However, it is conceivablethat the introduction of protein synthesis made these changes possible, as itprovided protein catalysts for replication and a strong selection for the use ofribosomes for translation. Both processes, translation and replication, had to bemade to function on the same template in opposite directions. The function of thesame template in both replication and translation seems not to be a major obstacle,as it occurs in all present-day viruses in a coordinated and regulated fashion.Another model for the early role of tRNAs proposed byWeiner andMaizels is the

terminal taging of the replicating RNAs. These terminal tags would have func-tioned as the selective binding and initiation site of the replicase and thereby wouldhave helped to replicate the genomic ends correctly. This hypothesis is supportedby the fact that many present-day viruses have tRNA-like 3’ termini and thetelomerase enzyme that synthesizes the ends of the eukaryotic chromosomesfunctions on a tRNA-like template.

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4.6The RNA World

Logically, it is necessary to assume that prior to the invention of protein synthesis,all reactions required for maintenance of macromolecules – and for their evolutiontowards life – had to be mediated by molecules other than proteins. Present-dayRNA chemistry has demonstrated that different RNA molecules (either naturalones or selected in vitro) may mediate several different catalytic activities, althoughthe RNA catalysts typically function less efficiently than protein enzymes, i.e., at amuch slower rate (Fig. 4.2). Such molecules are called RNA enzymes or ribozymes.Most of the naturally occurring ribozymes mediate cleavage and ligation reactionsof their target RNAs (Table 4.3). The smallest ribozymes contain about 50 nucleo-tides and occur in the RNAs of viroids and viral satellite RNAs, while complexribozymes capable of many different catalytic functions can be artificially producedby in vitro selection.It must be emphasized that the functionality of the RNA catalysts is based on the

sequence information. The information does not code for any protein products, butit dictates the folding of the RNA into secondary structures that can recognize theirsubstrates and cause the desired reactions. Figure 4.10 shows the three-dimen-sional folding structure, the so-called hammerhead structure, of the smallestnatural ribozymes, which are composed of about 50 nucleotides.Figure 4.11 gives an example of the evolution of an RNA polymerase ribozyme,

as mediated by in vitro selection steps. The class I ligase ribozyme catalyzes thejoining of the 3’ end of an RNA strand to the 5’ end of the ribozyme (Fig. 4.11 a);the class II ligase ribozyme catalyzes the addition of three nucleotide 5’ triphos-phates (NTPs) to the 3’ end of the primer, directed by an internal template

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Fig. 4.10 Three-dimensional folding structure(so-called hammerhead structure) of the small-est natural ribozymes. These self-cleaving and-ligating structures occur in several viroid andviral satellite RNAs and are composed of about50 nucleotides.

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(Fig. 4.11 b); finally, the class I–derived polymerase catalyzes the addition of up to14 NTPs on an external RNA template (Fig. 4.11 c).The hypothetic stage of early evolution, when all biochemistry was mediated by

different RNA catalysts, is called the RNA world. Invention of genetically encodedproteins brought out the new, protein-based biochemistry that soon replaced RNA-mediated catalysis. A curious example of this transition to protein-mediatedfunctions is that still today some proteins functioning in the regulation of trans-lation – namely, some translation elongation factors – are folded into a secondarystructure similar to that of the tRNAs. Apparently, after the RNA genomesaccumulated adequate coding capacity, the protein enzymes were able to convertthe RNA genomes to DNA form. Being much more stable than the RNAs, thesecould evolve into much larger sizes and superior coding capacity.With these immense improvements in biochemical functions, the original RNA-

mediated biochemistry might have disappeared without leaving a trace. However,this did not happen, as we do still have some clear molecular relicts, or molecularfossils, that apparently have been conserved from the RNA era into present-day life.The most convincing molecular fossil from the RNA world is that the primarygenetic code is still translatable only from RNA sequence (DNA exists only as aninformation storage system, comparable to a hard disk, containing all the data butno running program for translating this information). Further, the translationreaction, or the formation of the peptide bond, is still mediated by one RNAcomponent of the ribosomes, and the tRNAs still bring the amino acids into thetranslation reaction. Several other small functional RNAs exist in present-day cells(Table 4.3) and also may be functional relicts from the early RNA era.As mentioned in Section 4.3, some of these RNA catalysts – particularly those

that function in the maturation of different RNAs, especially small nuclear RNAsand nucleolar RNAs – as well as RNA-containing telomerase enzymes still occur in

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Fig. 4.11 Evolution of an RNA polymeraseribozyme mediated by in vitro selection steps.(a) The class I ligase ribozyme catalyzes thejoining of the 3’ end of an RNA strand (openline) to the 5’ end of the ribozyme; (b) theclass II ligase catalyzes the addition of three

nucleotide 5’-triphosphates (NTPs) to the3’ end of the primer, directed by an internaltemplate; (c) the class I–derived polymerasecatalyzes the addition of up to 14 NTPs on anexternal RNA template (from Joyce 2002, withpermission from the publisher).

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the eukaryotic organisms (Table 4.3). This suggests that those (slow) RNA-medi-ated functions have been maintained in eukaryotes from the times of RNA-basedlife. In prokaryotes, many RNA-processing functions have been replaced by pro-tein-catalyzed functions, apparently due to their adaptation to faster replication andto more efficient RNA processing, particularly in hot environments. For thesereasons it might be thought that the eukaryotic genome type – although expandedto huge sizes and complex gene sets over time – would be of a more ancient typethan the small and sophisticated prokaryote genomes.

4.6.1Origin of the RNA World

4.6.1.1 Prebiotic Assembly of PolymersIn order to get the functional RNA world started, preexistence of RNA polymerswas required. These RNA polymers supposedly appeared by spontaneous assemblyor polymerization of nucleotide monomers. They had to accumulate to significantamounts, and be of considerable length and variation, to ensure that this randomcollection contained some (or even one) that had the potential of copying itself and,later, of copying even other RNAs.The prebiotic, i.e., spontaneous, polymerization of RNA nucleotides is difficult to

explain with known RNA chemistry, because nucleotide polymerization requiresenergy and does not happen easily (see Chapter 3). It has been intensively studied –e.g., in the laboratory of James Ferris – and in these optimized conditions,polymers of about 40–50 nucleotides were produced. Such polymerization resultshave been obtained by allowing activated nucleotides to react in aqueous solutionin the presence of clay minerals, which significantly enhanced the polymerization.The enhancement by clays is caused, assumedly, by their fine-layered structure,composed of mineral grains with di- and trivalent positive charges. Those cationicsurfaces bind and immobilize the negatively charged nucleotides, placing them insuitable positions to promote their reactions with each other. Further on, bindingto the clay surfaces significantly stabilizes the ready-made RNA polymers, whichotherwise would be very easily degraded by hydrolysis.The group of Deamer reports that another environment that promotes RNA

polymerization, although to a lesser extent than clays, is the eutectic (very cold) icesolutions; an icy environment is also known to promote the ribozyme-catalyzedligation of RNAs. The liquid water phase remaining in between ice crystalsconcentrates the precursors effectively, and the low temperatures help to slowdown the reacting components to allow the formation of the phosphodiester bondsbetween nucleotides.For building the nucleotide polymers, the nucleotides need to be linked to each

other via phosphodiester bond between the 3’ and 5’ carbons of the adjacent sugars(Fig. 4.3). For this, the nucleosides first have to be phosphorylated at their5’ carbon. In the early world this was problematic because soluble phosphateswere not readily available. It is possible that the inorganic phosphate dissolved inlow amounts from calcium phosphate (hydroxyapatite) mineral or from volcani-

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cally produced linear polyphosphates, or from their breakdown products, andphosphorylated nucleosides to nucleotides. But this reaction is difficult and mightoccur only in the presence of urea, ammonium chloride, and heat.Polymerization of the nucleotides requires that they be activated by some high-

energy bond at the 5’ position to provide energy for the uphill reaction. In present-day life, this binding energy is obtained from the hydrolysis of the triphosphatemoiety, but this was not adequate in the prebiotic world because triphosphatesalone do not promote (non-enzymatic or non-catalyzed) polymerization. Therefore,it seems that the nucleotides had to be charged with other available molecules, suchas amino acids, bound with high-energy bonds at the 5’ position of the phosphory-lated nucleotides. The most effective activating groups, now commonly used forthe polymerization experiments in laboratories, are the different phosphorami-dates, such as phophoramidazoles. These compounds are formed from nucleoside5’ polyphosphates and amines or imidazoles; but such complex activating groupsmight not have been available in the prebiotic environment.A further complication in the polymerization of ribonucleotides is that in a

mixture of monomers, several different reactions take place. To make a functionalpolymer, the monomers must form the mono-phosphodiester linkage exactlybetween the 3’ and 5’ carbons of the adjacent nucleotides. However, the ribosering has reactive groups in carbons at positions 5’, 3’, and 2’ (Fig. 4.3). In prebioticconditions all these groups could react with each other, and cyclic compoundscould be formed between the 2’ and 3’ OH groups. Furthermore, the phosphatemolecules might have formed different polyphosphate linkages between differentcarbons. All these varying bonds would have produced dead-end products forfurther polymerization. It is still unclear what kind of conditions promoted thenucleotides to react in an orderly fashion to produce only the correct, 3’-to-5’-linkedRNA polymers (Fig. 4.4).

4.6.1.2 The Building Blocks of the RNA WorldFor synthesis of nucleosides, the purine bases adenine and guanine (A and G), thepyrimidine bases cytosine and uracil (C and U), and the D-isoform of cyclic ribosesugar are needed. Prebiotic synthesis and assembly of these nucleoside buildingblocks have been intensively studied by groups of chemists led by Gerald Joyce,Stanley Miller, Leslie Orgel, and Alan Schwartz. The prebiotic synthesis of thesecomponents, as well as the prebiotic synthesis of their small organic precursorssuch as CH4, NH3, CH2O, CNH, CN2H4, C3NH, CH2O, CN2H4O, and SH2, iscovered in Chapter 3.Provided that ribose sugar and the nucleobases were available, further on the

bases had to be covalently linked in �-orientation with the 1’ carbon of ribose toform nucleosides. This reaction may be activated by heating and it produces purinenucleosides, although with very low yield. Routes for prebiotic synthesis of pyr-imidine nucleosides are not well known, but they may be feasible via multiplesugar phosphate intermediates. Recently, a completely different route has beenfound, where Æ-D-cytosine was produced directly from ribose sugar and hydrogen

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cyanide. This efficient reaction thus produced cytosine, even if of the wrongisoform, and it also converted the existing (unstable) ribose into a stable form.Prebiotic synthesis of nucleotides would have yielded a racemic mixture of a

variety of different nucleotide analogues, both in Æ and � and in L- and D-isoforms.A spontaneous polymerization reaction of such (randomly) phosphorylated nu-cleotides would have been very slow and would have led to a wide variety ofdifferent linkages, formed between the whole variety of different nucleotide ana-logues and isoforms. Such randomly linked oligomers or polymers would not havebeen extendable or functional as templates for replication.Altogether, prebiotic formation of RNA nucleotides and their polymers, starting

from small molecular precursors such as HCN, NH3, CH2O, CH4, PO43–, or H2O,

involves so many unlikely or adverse chemical steps that many chemists havespeculated that RNA synthesis had to be preceded by simpler chemical polymers –or by nucleic acid analogues whose backbone is composed of non-chiral structures.Polymers proposed as hypothetical predecessors of the RNA world include peptidenucleic acids (PNAs) with a peptide as backbone, threose nucleic acids (TNAs), andpyranosyl-derived nucleic acids (p-RNAs) (see Chapter 1). If any of these polymerswas a direct precursor of present genetic material, then it must have been possibleto transfer the information by copying or transcription from this molecule intoRNA or DNA sequence, which indeed has been experimentally demonstrated forPNAs. However, the role of other polymers in the early steps of molecularevolution does not seem very plausible, because the central molecules of earlylife (the ribosomes and tRNAs) are based solely on RNA molecules.To find possible solutions for the appearance of the nucleotide-based (very

complex) genetic information, Cairn-Smith (1982) has postulated that instead oforganic polymers, entirely different molecules, such as minerals, may have con-tained the earliest pre-genetic (replicating) information. Still, it is not clear how anyspecific information would have been coded in the crystal structure of mineralsurfaces, or how these would have been converted to be biologically significant.Little is known, as yet, of what the available starting materials were, what theconditions were where the prebiotic chemistry took place, and what chemical andphysical reactions and selection processes were driving the increasing complexityof the early polymers (see also Chapter 1).

4.6.1.3 Where Could the RNA World Exist and Function?The question of the possible location and conditions of the proposed RNA world isvery difficult. It is assumed that the initial RNA polymers were formed by randompolymerization of nucleotides, but this scenario requires that the nucleotides hadto be initially available in the environment. Further on, for the synthesis ofnucleotides, their precursors – ribose sugar, purines and pyrimidines, and phos-phate molecules – had to be available. For the prebiotic synthesis of those com-pounds, their precursors or the small organic molecules such as CH2O, CNH,CN2H4, and HNCO had to be available in adequate amounts. To drive repeatedpolymerization reactions, leading to significant accumulation of the products

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(adequate for starting a whole new polymerization and replication network), a long-term, high-level supply of nucleotides would be required.The prebiotic synthesis or at least the accumulation of nucleotides would need to

happen in conditions where, further on, the nucleotides could spontaneouslypolymerize. The conditions also should have been adequately gentle to maintainthe polymers intact. The prebiotic synthesis of some of the precursors happenspreferably in cold or mildly warm conditions (synthesis of nucleic acid bases),while other steps require heat (nucleoside formation and phosphorylation). So it isconceivable that the locations for the different steps may have been temporally orlocally separate.The polymerization of nucleotides needs to take place in an aqueous environ-

ment because the nucleotides are water-soluble and liquid water is needed to carrythem into the reaction site. However, water efficiently reacts with the RNApolymers to hydrolyze the phosphodiester bonds, which breaks up the polymers.The hydrolysis reactions occur faster at higher temperatures; therefore, cool, closeto freezing temperatures would be more suitable for preserving RNA polymers.A further complication arises with the templated polymerization – meaning the

copying or replication of existing RNA strands. Because the phosphate groupsforming the phosphodiester bonds carry a negative charge of –1, the total chargeof the polymer is highly negative. In the templated replication, the complementarystrand is assembled on the existing template by hydrogen bonding between thecomplementary nucleotides (A to U andG to C) (Fig. 4.4). For stable assembly of thecomplementary strand, the negative charges of the phosphates need to be neutral-ized by an adequate level of soluble cations (positive ions). This neutralizationtogether with the hydrogen bonding of the bases leads to a stable assembly, andthe double-stranded product is closed for any further assembly of new strands on thesame templates. Thus, the double-stranded structure could be a dead-end product.To avoid this, some energy input or radical change of environment – e.g., by

dilution out of the cationic ions or warming up of the solution – would be needed toopen up the double helix. Lathe (2005) has proposed that alternating conditions oflow and high salt concentrations (as in tidal pools) would be needed to drive theassembly and separate the daughter strands. Brown and coworkers have experi-mentally shown that efficient melting (i.e., separation) of double-stranded nucleicacid strands can be obtained by convection-driven cycling of molecules in micro-compartments located in steep temperature gradients, such as the tiny compart-ments in the FeS precipitate mounts of hydrothermal vents.Still another putative environment that might have driven prebiotic chemistry

and the assembly of macromolecules, possibly including polymers, is the sandy orsilty beaches washed by the ocean tides. Bywater and Conde-Frieboes (2005) haveproposed that in these locations the ocean water would have brought in theprecursors for the reactions, and these might have been bound, by hydrogenbonding or ionic forces, to the cationic minerals in the clay and sand. Small dryingponds might have provided the concentration mechanism for the compounds, andthe subsurface layers of sand might have provided protection against UV radiation,as well as size-based fractionation and concentration by chromatographic filtration.

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The clay-like minerals would have been suitable catalytic surfaces for the assemblyof nucleotide polymers. The repeated washes by new waves or tides might haveprovided the cyclic dilution effects needed for the separation of the replicatingnucleotide strands, as proposed by Lathe.

4.7Beginning of Life

The above discussion should indicate that the origin of life was by no meanssimple. Rather, it should have been a procession through multiple stages ofspontaneous – but most often uphill – reactions of molecular chemistry andevolution towards cellular life. Within this procession it is difficult to determinewhen life actually started. It seems that there was a stage where the developingsystem was not yet clearly alive, and also no longer clearly lifeless, but swaying inbetween different directions of development in a type of bifurcating stage. Such athreshold level could have been achieved when the first sequences could replicatethemselves but when there were no biosynthesis pathways, as yet, for any of theprecursors or building blocks for making more of the same molecules. The systemwas modified and adapted by a selective evolution, but it was still wholly dependenton the supply of complex materials from its environment. It is conceivable thatsuch a threshold stage could have developed in several directions: one, for instance,to produce the semi-living (replicating but not autonomous) viral world andanother to produce autonomous cellular life. Parasitic and synergistic interactionsalso evolved – the viruses ending up as parasites of cellular life – but the earlymolecular interactions may have been more varied.The question of the beginning of life is related to how we define life. Life, as we

now know it, is very complex and versatile, but the definition should include justthe very minimal and first features that were required of a system to become alive.Andr� Brack has defined primitive life as an aqueous chemical system able totransfer its molecular information and to evolve (see Chapter 1). Eigen hasdescribed life as phenomena in the multidimensional information space, wherethe species – or quasi-species – form as their genomic sequences accumulate in theproximity of the optimal or best-adapted sequence, at so-called “fitness peaks.”Both these descriptions emphasize the information-driven nature of life, themaintenance of information via replication, and accumulation of new informationvia natural selection and evolution.In a reductionist way, it might be claimed that genomic information is the

essential part of life and that the cellular structure serves only as a vehicle tomaintain and renew the information. But the cellular structure has played a centralrole in the formation of information: the accumulated information just reflects theneeds of the cells, and the optimized information is determined by the adaptationof the cell to its environment.The very initial functional information appeared by accident, as a random

sequence was able to replicate itself. The further accumulation of information

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took place via improvement of that very function. When the system grew andevolved, new functions were “invented” that allowed the system to survive better inits environment. The selection, or genetic adaptation, was mediated via differentinteractions. Intracellular molecular interactions were, and still are, of essentialimportance, as were the interactions of the cell with its surroundings, with themembers of its own species, and with the whole surrounding ecosystem. Theseinteractions are the driving force for the accumulation of genetic information.Even the simplest cellular life is mediated via multiple biochemical reactions

driven by energy conversion reactions and, ultimately, by energy drawn from asuitable energy source. With these, life achieves a remarkable organization ofmatter and energy. The cellular structure is essential for the containment of allthese reactions and for the assembly of the organized structures.Thus, life is indeed based on genetic information and on evolution, but the third

essential party in the assembly of life is its cellular form. The cell and its inter-actions with the environment – and, on the other hand, its separation from theenvironment –build the entity that has allowed the accumulation of informationand that has facilitated evolution, and the self-sustained existence of the organism.Its existence still depends on suitable energy sources and availability of nutrients,i.e., on the life-supporting environment. A cell, adapting in its life-supportingenvironment, was the last defining requirement for the establishment of life aswe know it on Earth.

4.8Further Reading

4.8.1Books

Brack, A. The Molecular Origin of Life.Assembling Pieces of the Puzzle, CambridgeUniversity Press, Cambridge, 417 pp.,1998.

Cairn-Smith, A. G. Genetic Takeover and theMineral Origins of Life, Cambridge Univer-sity Press, Cambridge, 1982 (http://origin-oflife.net/cairns_smith/).

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4.8.2Articles in Journals

Abe, Y. Physical state of the very early earth,Lithos 1993, 30, 223–235.

Berclaz, N., Muller, M., Walde, P., Luisi,P. L. Growth and transformation of vesiclesstudied by ferritin labeling and cryotrans-mission electron microscopy, J. Phys. Chem.2001, 105, 1056–1064. (http://www.plluisi.org/)

Biebricher, C. K., Eigen, M. The error thresh-old, Virus Res. 2005, 107, 117–127.

Bywater, R. P., Conde-Frieboes, K. Did life beginon the beach? Astrobiology 2005, 5, 568–574.

Chang, I.-F., Szick-Miranda, K., Pan, S., Bailey-Serres, J. Proteomic characterization of evo-lutionary conserved and variable proteins ofArabidopsis cytosolic ribosomes, PlantPhysiol. 2005, 137, 848–862.

Chen, I. A., Roberts, R.W., Szostak J.W. Theemergence of competition between modelprotocells, Science 2004, 305, 1474–1476.

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Delaye, D. Becerra, A., Lazcano, A. The lastcommon ancestor: what’s in the name, Orig.Life Evol. Biosph. 2005 35, 537–554.

DeDuve, C. A research proposal on the originof life, Orig. Life Evol. Biosph. 2002, 33,559–574.

Deamer, D., Dworkin, J. P., Sandford, S.A.,Bernstein, M. P., Allamandola, L. J. Thefirst cell membranes, Astrobiology 2002, 2,371–381.

Doolittle, W. F. Phylogenetic classification andthe universal tree, Science 1999, 284, 2124–2128.

Eigen, M. The origin of genetic information:viruses as models, Gene, 1993, 135, 37–47.

Ferris, J. P. Montmorillonite catalysis of 30–50mer oligonucleotides: laboratory demon-stration of potential steps in the origin of theRNA world, Orig. Life Evol. Biosph. 2002, 32,311–332.

Forterre, P. The two ages of the RNAworld, andtransition to theDNAworld: a story of virusesand cells, Biochim. 2005, 87, 793–803.

Forterre, P., Confalonieri, F., Charbonnier, F.,Duguet, M. Speculation on the origin of lifeand thermophily: Review of available infor-mation on reverse gyrase suggests that hy-perthermophilic procaryotes are not soprimitive, Orig. Life Evol. Biosph. 1995, 25,235–249.

Gil, R., Silva, F. J., Pereto, J., Moya, A. Deter-mination of the core of the minimal bacte-rial gene set. Microbiol. andmolec, Biol. Rev.2004, 68, 518–537.

Hanczyc, M.M., Szostak, J.W. Replication ofvesicles as models of primitive cell growthand division. Current Opin., Chem. Biol.2004, 8, 660–664.

Jeffares, D. C., Poole, A.M., Penny, D. Relictsfrom the RNA world, J. Mol. Evol. 1998, 46,18–36.

Joyce, G. F. The antiquity of RNA-based evo-lution, Nature 2002, 418, 214–221.

Kanavarioti, A., Monnard, P.-A., Deamer,D.W. Eutechtic phsces in ice facilitate non-enzymatic nucleic acid synthesis, Astrobiol-ogy 2001, 1, 271–281.

Kapp, L. D., Lorsch, J. R. The molecular me-chanics of eukaryotic translation, Ann. Rev.Biochem. 2004, 73, 657–704.

Koonin, E., Martin, W. On the origin of ge-nomes and cells within inorganic compart-ments, Trends Genet. 2005, 21, 647–654.

Lathe, R. Tidal chain reaction and the origin ofreplicating polymers, Int. J. Astrobiol. 2005,4, 19–31.

Lehto, K., Karetnikov, A. Relicts and modelsof the RNA world, Int. J. Astrobiol. 2005, 4,33–41.

Liang, H., Landweber, L. F. Molecular mimi-cry: quantitative methods to study structuralsimilarity between protein and RNA, RNA2005, 11, 1167–1172.

Maizels, N., Weiner, A.M. Phylogeny fromfunction: evidence from the molecular fossilrecord that tRNA originated in replication,not translation, Proc. Natl. Acad. Sci. USA1994, 91, 6729–6734.

Martin, W., Russell, M. J. On the origin of cells:a hypothesis for the evolutionary transfor-mation from abiotic geochemistry to che-moautotrophic prokaryotes, and from pro-karyotes to nucleated cells, Phil. Trans. R.Soc. Lond. B. 2002, 358, 59–85 (also in:www.gla.ac.uk/project/originoflife/html/2001/pdf_files/Martin_&_Russell.pdf).

Mojzsis, S. J., Arrhenius, G., Keegan, K. D.,Harrison, T.M., Nutman, A. P., Friend,C. R. L. Evidence for life on Earth before3,800 million years ago, Nature 1996, 384,55–59.

Orgel, L. E. Prebiotic chemistry and the originof the RNA world, Crit. Rev. Biochem. Mo.2004, 39, 99–123.

Pennisi, E. Is it time to uproot the tree of life,Science 1999, 284, 1305–1307.

Poole, A., Penny, D., Sjçberg, B-M. Methyl-RNA: an evolutionary bridge between RNAand DNA? Chem. Biol. 2000, 7, R207–R216.

Poole, A., Jeffares, D., Penny, D. Early evolu-tion: prokaryotes, the new kids on the block,BioEssays 1999, 21, 880–889.

Poole, A.M., Jeffares, D., Penny, D. The pathfrom the RNA world, J. Mol. Evol. 1998, 46,1–17.

Sanders, P. G.H. Chirality in the RNA worldand beyond, Int. J. Astrobiol. 2005, 4, 49–61.

Schmidt, G., Christensen, L., Nielsen, P. E.,Orgel, L. E. Information transfer from DNAto peptide nucleic acids by template-directedsyntheses, Nucleic Acids Res. 1997, 25, 4793–4796.

Steitz, T. A., Moore, P. B. RNA, the firstmacromolecular catalyst: the ribosome is aribozyme, Trends Biochem. Sci. 2003, 28,411–418.

4.8 Further Reading 119

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Tian, F., Toon, O. B., Pavlov, A. A., De Streck,H. The hydrogen-rich early atmosphere,Science 2005, 308, 1014–1017.

Vlassov, A. V., Johnston, B. H., Landweber,L. F., Kazakov, S.A. Ligating activity offragmented ribozymes in frozen solution:implications for the RNA world, Nucl. AcidsRes. 2004, 32, 2966–2974.

W�chtersh�user, G. From pre-cells to Eukarya– a tale of two lipids,Mol. Microbiol. 2003, 47,13–22.

Watson, E. B., Harrison, T.M. Zircon ther-mometer reveals minimum melting condi-tions on earliest Earth, Science 2005, 308,841–844.

Weiner, A.M., Maizels, N. The genomic taghypothesis: modern viruses as molecular

fossils of ancient strategies for genomicreplication, and clues regarding the originof protein synthesis, Biol. Bull. 1999, 196,327–330.

Westall, F. Life on the early Earth: A sedi-mentary view, Science 2005, 308, 366–367.

Woese, C. R. The universal ancestor, Proc. Natl.Acad. Sci. USA 1998, 95, 6854–6859.

Woese, C. R., Kandler, O., Wheelis, M. L. To-wards a natural system of organisms: Pro-posal for the domains Archaea, Bacteria andEucarya, Proc. Natl. Acad. Science USA 1990,87, 4576

Yang, S., Doolittle, R. F., Bourne, P. E. Phy-logeny determined by protein domain con-tent, Proc. Natl. Acad.Sci. USA 2005, 102,373–378.

4.9Questions for Students

Question 4.1What are the difficulties in understanding of the origin of life?Question 4.2

What are the building blocks of life and how do they assemble to make functionalcells?Question 4.3

What are the putative steps required for the establishment of self-sustainable life?Question 4.4Explain the RNA world.Question 4.5What kind of conditions might have driven the prebiotic molecular evolution

towards life?Question 4.6What can we say of the LUCA and of the differentiation of the three domains of

life from LUCA?Question 4.7How do you define the beginning of life?

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4From Molecular Evolution to Cellular LifeKirsi Lehto

In this chapter, contemporary cellular life is analyzed in order tosee which components are the most ubiquitous and conserved inall life forms and therefore assumed to be the most original func-tional units of life. Molecular analysis of these structures givessuggestions of how they were involved in early molecular evolutionand what functions they may have provided to the early (pre-cellular) replicators. By going backwards, step by step, one seeswhich inventions had to precede each stage of early evolution:genetically encoded proteins had to exist prior to the establishmentof the Last Universal Common Ancestor (LUCA), and RNA repli-cators, or replicating RNA analogues had to predate geneticallyencoded proteins. Special attention is given to the most conservedcomponents of the present life forms, considered to be relicts of theearly RNA world.

4.1History of Life at Its Beginnings

Our home planet was formed about 4.6 billion years ago. The initial conditions onthe young planet Earth were very harsh. The accretion process had heated theprotoplanet, and the temperature of the young planet was further increased by thegreenhouse phenomena caused by the dense atmosphere formed by H2O and CO2

and by continuing impacts from the colliding comets and meteorites. The initialplanet temperature was hot enough to keep the Earth’s crust in liquid form,forming a magma ocean on the surface. As the planet radiated heat, the temper-ature was reduced; when it came down to about 200 �C, with the prevailing highatmospheric pressure, the water vapor precipitated and rained down to formoceans. The dating obtained from the oldest zircon crystals indicates that liquidwater was present on the planet 4.4 billion years ago. The first Earth crust formed

4.1 History of Life at Its Beginnings 85

Complete Course in Astrobiology. Edited by Gerda Horneck and Petra RettbergCopyright � 2007 WILEY-VCH Verlag GmbH & Co. KGaA, WeinheimISBN: 978-3-527-40660-9

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underneath the water. Because of heavy cometary and asteroid impacts, the con-ditions on Earth remained hot and violent for perhaps 500 million years; this timeis called the Hadean period.Conditions during the Hadean period are difficult to investigate because all the

rocks formed during that era have been thoroughly metamorphosed by the tectonicprocesses of the later times. The oldest still existing sedimentary rocks are locatedat Isua, Greenland, and date back to about 3.8 billion years. These rocks containsmall granules of sedimented carbon, which is specifically enriched in the 12Crather than the heavier 13C isotope. The enrichment of the lighter carbon isotope inthese sediments suggests that the carbon was once bound in biologically producedcompounds (see Chapters 1 and 2). The real biological origin of these carbondeposits has been questioned, but other nearly as old samples containing 12C-enriched carbon and fossilized microbial structures have been detected at two otherlocations: in the 3.5-billion-year-old sediments at Pilbara, western Australia, and atBarberton, South Africa. These findings suggest that life was well established, andapparently widely distributed on the Earth, at this very early stage – or soon afterthe heavy bombardment ended and the planet cooled to temperatures conducivefor life. It is not known at what temperature regimes life started. The mostthermotolerant contemporary life forms are known to propagate in temperaturesup to 113�C (see Chapter 5), but the prebiotic replicating macromolecules, and alsothe earliest cellular structures, may have been rather fragile and sensitive forhydrolytic conditions and most likely were not durable in very high temperatures.Since its early start, life has spread and diversified and now occupies all con-

ceivable ecological niches on the Earth (see Chapter 5). During its spread andaccumulation, life has also modified the environment and has profoundly changedthe conditions on planet Earth, including the chemical composition of the atmos-phere, the oceans, and the Earth’s crust. The long-term geological processes oftectonics, volcanism, weathering and erosion, as well as degrading processescaused by life itself, have completely reshaped and mixed multiple times theconditions that prevailed on the early Earth and have abolished most of thechemical and geochemical traces that were formed at this early time. Therefore,there are not any direct data of the conditions that once allowed or induced theorigin of life. It is even not know in what type of locations on Earth – or, potentially,on nearby planetary bodies – life did start. Thus, trying to trace back the veryearliest stages of this process becomes difficult and speculative.However, different scientific approaches may be used to try to resolve what kind

of conditions and what chemical compounds might have driven the life-producingreactions. Clearly, the origin of life has been a very complex process and needs to bestudied in many different fields of science. Astronomy is needed to resolve how theelements, the Solar System, and the planet Earth were formed in the first place.Geosciences are needed to resolve the conditions on the early Earth and thecomposition of the early atmosphere, the ocean, and the crust. Inorganic andorganic chemistry are needed to resolve how the elements, inorganic minerals, andvolatiles may have reacted to form small organic compounds and more complexorganics such as nucleotides and amino acids, which are the building blocks of life.

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Further on, the quest is to resolve how these organic molecules may polymerizeand, in particular, how these reactions might conceivably have happened in pre-biotic conditions in the absence of genetically encoded enzymes and biochemicalreactions.Present-day life is solely driven by multiple protein-catalyzed (-mediated) bio-

chemical reactions and complex molecular interactions. The fields of biochemistryand bioinformatics study how these enzymes and other proteins now function andhow they have changed over the evolution of life. These studies can identify thegenetic sequences that are the most conserved (i.e., the oldest and most originalones) in different life forms. Of particular interest here are the reactions that stillare catalyzed not by proteins but by different RNA molecules. Such RNA enzymes(or ribozymes) may be derived from the very oldest life forms or from the erapredating the DNA-protein-based life forms.As a central part of the study of life, different fields of biology study the essential

structures and functions of life; how life reacts and adapts in its environment; andhow all functions are mediated, regulated, and coordinated on the cellular andmolecular level. All these integrated efforts are needed to construct an under-standing of what life is, how it has evolved through times, and, maybe, how itstarted in the first place.It may be assumed that the chemical and molecular evolution towards life

proceeded through a long cascade of different stages, initiated by spontaneousreactions between abundant chemical elements, or the chemical constituents oflife: carbon, hydrogen, oxygen, nitrogen, sulfur, and phosphor (C, H, O, N, S, P). Insome high-energy conditions these elements formed reduced carbon and nitrogencompounds, such as hydrogen cyanide (HCN), ammonia (NH3), methane (CH4),and formaldehyde (HCHO). In suitable conditions these small organic molecules,together with water (H2O), reacted to form the building blocks of life: the nucleicacid bases (purines and pyrimidines), sugars and other hydrocarbons, and aminoacids (see Chapter 3 and Section 4.2). These, again via multiple chemical reactionsand interactions (which are not well understood as yet), formed polymers andmore-complex molecules. Some of the polymers gained the chemical potential tocopy themselves or to replicate, which was the first major transition towards theorigin of life. Replication initiated molecular evolution, which led to the inventionof genetically encoded proteins and, eventually, to the appearance of the firstcellular life forms. From then on, the diversification of life into all the species ofthe biosphere has been covered by Darwinian evolution.This chapter aims to trace back this process in order to visualize the different

stages of the progress from early organic molecules to cellular life forms. Instead ofstarting from the very beginning and progressing upwards, the chapter starts fromthe central features of cellular life as they are known now, because it is known forcertain that this is what eventually came out of early evolution (at the time ithappened, evolution was random and not directed – the outcome could be knownonly after it had happened). Then proceeding backwards, step by step, it discusseswhat types of simpler forms could have given rise to each of the new and morecomplex innovations.

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4.2Life as It Is Known

4.2.1The Phylogenetic Tree of Life

Life is characterized by endless complexity. On the visible level one can observe themultitude of genera, species, forms, and individuals, each thriving in their owntypical ecological niches. Cells of higher organisms are differentiated into organsand tissues, which each present their specific form and function even that they allare regulated by the same genome of the same individual. Variation of species andsubspecies in the microbial world is vastly larger than that of the macrospecies. Themicrobial species can be separated into three different domains of life. Single-celledorganisms such as yeasts, ciliates, and flagellates, which do posses a nucleus in theircells, together with all the higher organisms belong in the domain of Eukarya. Thecells that do not posses a nucleus belong to the prokaryotes, which again belong totwo distinct domains, the Bacteria (or by older nomenclature, the Eubacteria) andthe Archaea (older name, the Archaebacteria). These three domains of life (Eukarya,Bacteria, andArchaea) each constitute their own and separate lineages of life and canbe distinguished from each other by multiple genetic and biochemical markers.The three domains of life share a large number of common features that are

ubiquitous to life, or are the same or very similar in all living organisms. It isbelieved that these features were inherited from a common ancestor of all lifeforms, the Last Universal Common Ancestor (LUCA). However, the properties ofLUCA at the time of diversification and the exact sequence of the separation of thethree lines are still unclear. Clearly, the common ancestor has developed through acascade of gradually increasing complexity, and it is not quite clear, which stagewas The Last Common One. As reviewed by Delaye and coworkers (2005), it mighthave been a community of simple precursors of life, the so-called progenotes (seeSection 4.3.2), or even a community of free-living replicating molecules, predatingthe establishment of cellular life. However, recent phylogenetic studies (i.e.,studies of the lineages and relatedness of known organisms through statisticalcomparison of their genetic sequences) by, e.g., the groups of Lazcano andDoolittle, indicate that LUCA was a well-established cell line. The properties ofLUCA will be discussed below.

4.2.2Life is Cellular, Happens in Liquid Water, and Is Based on Genetic Information

From unicellular microorganisms to all higher life forms, all life on Earth iscellular (Fig. 4.1). Prokaryotes are single-celled organisms. The cells are simpleand usually devoid of any internal membrane structures (except for the photo-synthetic cyanobacteria, which possess intensive photosynthetic membranes). Thecells are spherical, ellipsoid, elongated, or rod-shaped (see Chapter 5) and of sizesvarying from 0.1 �m to 600 �m, depending on the species.

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All eukaryote cells have intensive internal structure. Cell organelles include• the nucleus (contains the chromosomes or the genomic

DNA);• mitochondria (energy-producing organelles);• the endoplasmic reticulum (internal membranes),• the Golgi apparatus (membranous vesicles for protein pro-

cessing and transport),• lysosomes and peroxisomes (for containment of degradative

enzymes and wastes); and• chloroplasts (photosynthetic organelles; in plant cells only).

The cells of all eukaryotes are very similar to each other, except that the plant cellshave thick and rigid cell walls and contain numerous chloroplasts (or other types ofplastids). Typical sizes vary from 10 �m to several hundred micrometers, but somelarge cell types occur (of a size up to more than 1 m for some nerve cells).Multicellular organismsmay be conceived as tightly bound colonies of individual

cells. The cells are entities contained within the cell membrane, which separates

4.2 Life as It Is Known 89

Fig. 4.1 All life is cellular. (A) Microscopic view of (unidentified)bacterial cells. (B) Scheme of a eukaryotic cell (animal cell on theleft, and plant cell, with a rigid cell wall, on the right) showing theintensive internal structure.

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the cell from its environment but also allows sophisticated communication withthe environment. The communication includes the intake of water and necessarynutrients, excretion of waste products, receiving of chemical signals via differentreceptor molecules, and sending off signals via secretion of different molecules.Thus, the cells dynamically communicate with their environment. All communi-cation through the membrane is mediated via specific proteinaceous channels andstructures embedded in the membrane, because the membrane itself is a hydro-phobic barrier and therefore impermeable to water-soluble molecules.Inside the cells, life is a chemical process where multiple biochemical reactions

take place in aqueous solution. Water functions as the solvent and carrier for ionicand polar molecules, and also is a reacting component in many reactions. Wateralso serves as the exclusion medium to allow the lipid molecules to assemble andformmembranes, and as the medium that interacts with proteins, helping them tofold into their three-dimensional forms. Therefore, water provides a suitableenvironment for the different cellular reactions and for the assembly of importantcellular structures. It provides turgor (internal pressure) and strength to the cells.Water is such an essential environment and requirement for all the life functionsthat it seems likely that the origin of life had to happen in an aqueous environment(see Chapter 1).Proteins, or gene products, have a multitude of essential roles in the cells. They

form several different structures, such as the cytoskeletons in eukaryotes, com-ponents of cell walls, and the porous structures in cell membranes. They regulatereactions such as gene expression and genome replication, and they function insignal transduction by interacting with different target molecules. Still anotherarea where proteins are essential for life is in the (regulated) catalysis of all thereactions going on inside the cells. Most cellular molecules are both synthesizedand degraded via multi-step reaction pathways – and none of these reactionswould happen, at least at any desired rate, without the assistance of proteinaceousenzymes. Even the energy conversion and -releasing reactions have to be medi-ated via enzymatic catalysis so that they happen in a controlled and regulated

4 From Molecular Evolution to Cellular Life90

Fig. 4.2 Chemical reactionrates in dependence of sub-strate concentration, with andwithout enzyme catalysis. En-zymes speed up reaction ratesvery strongly as compared tonon-catalyzed reactions andmake them happen efficientlyeven at very low substrate con-centrations. The maximum rateof reaction is reached when theenzyme becomes saturatedwith the substrate molecules.

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fashion. The enzymes themselves do not participate in the reactions but associatewith the reacting molecules and hold them in such a conformation that thereaction can proceed. Enzymatic catalysis is capable of raising reaction rates bymany orders of magnitude, from nearly zero to very high, and in practice mostbiological reactions would not happen in physiological conditions without enzymecatalysis (Fig. 4.2).Proteins form the tools and the structures in the cells, and genetic information,

encoded in the genomic deoxyribose nucleic acid (DNA), specifies how these toolsand structures are made. Life depends on the function of the proteins and thus onthe genetic information coding for them. Proteins are composed of long chains ofdifferent amino acids, and the sequence of the amino acids in these chains isdetermined by the genes coding for them. From the DNA, the protein-codingsequences are first copied into ribose nucleic acid (RNA) and from this areconverted into amino acid sequences in peptide chains. RNA is a polymer moleculevery similar to DNA; it is composed of similar nucleotide components, with onlythe small difference of an OH group, rather than H, being connected to the carbonin position 2 (2’) in the pentose sugar ring (thus, the sugar is ribose instead of

4.2 Life as It Is Known 91

Fig. 4.3 Structure of the componentsof genetic material: the nucleic acidbases adenine, guanine, cytosine,thymine, and uracil; the deoxyriboseand ribose sugar molecules; and thephosphate moiety.

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deoxyribose) (Fig. 4.3). However, this OH group is very reactive and, differing fromthe DNA, makes the RNA polymers very fragile, unstable, and short-lived.

4.2.2.1 Genetic InformationThe complexity of life extends strongly to the molecular level, i.e., to the nucleicacid and protein level inside the cells. The genetic information is encoded in thegenomic DNA in the sequence of four different deoxyribonucleotides (or, in short,nucleotides), which are the phosphorylated form of adenosine (A), guanosine (G),cytosine (C), and thymidine (T) nucleosides. In RNA, the uridine nucleoside isused instead of the thymidine nucleoside. The nucleosides themselves are formedof the corresponding bases (adenine, guanine, cytosine, thymine, and uracil); ofthese, A and G bases are purines and C, T, and U bases are pyrimidines (Fig. 4.3).The bases are covalently bound to a deoxyribose (in DNA) or ribose (in RNA) sugarto form nucleosides. These are phosphorylated at the carbon at their 5’ position toform nucleotides, and these again are connected into long chains via phospho-diester bonds between the 5’ and 3’ carbons (these are the carbons in positions 3and 5 in the ribose ring) of the adjacent sugars (Fig. 4.4).The number of nucleotides in the genomes varies largely between different

species. The genomes of the smallest prokaryotes are composed of about 0.5 � 106

nucleotides, while the genome of the bacterium Escherichia coli is composed of4.8 � 106 nucleotides. The smallest eukaryotic genomes are about an order ofmagnitude larger, but the more complex ones are many orders of magnitude largerthan the prokaryote genomes. The genome of wheat, for instance, is composed of

4 From Molecular Evolution to Cellular Life92

Fig. 4.4 Schemes of DNA. (A) The deoxyribonucleotide polymerformed by diester bonds between the 3’ and 5’ carbons ofadjacent nucleotides; (B) the double helix of two DNA strandsshowing the base pairing of the nucleic acid bases.

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about 17 000 � 106 nucleotides, the human genome of 3 400 � 106 nucleotides, andthat of the fruit fly of 97 � 106 nucleotides (Table 4.1). Further, the number of genesvaries a lot, being about 400 in the smallest endosymbiotic bacteria (Buchneraaphidicola) and some hundreds of thousands in the largest genomes.

Table 4.1 Genome size and coding content of different types oforganisms.

Species Domain Genome size(million bp)[a]

No of genes Coding (%)

Mycoplasma genitalium Bacteria 0.58 470 100Escherichia coli Bacteria 4.8 4 288 100Methanococcus jannaschii Archaea 1.7 1 738 100Saccharomyces cerevisiae Eukarya 12 6 144 70Caenorhabditis elegans Eukarya 100 18 266 25Arabidopsis thaliana Eukarya 100 25 498 31Homo sapiens Eukarya 3 400 32 000 28[b]

1.4[c]

Triticum aestivum Eukarya 17 000 60 000 Not determinedAmoeba dubia Eukarya 670 000 Not determined

a Million base pairs = number of nucleotides.b Total.c For proteins.

The very large genomes, e.g., those of wheat or amoebas, have not been sequenced.Therefore, their accurate sizes and gene contents are not known as yet but can beestimated from their physical properties. It is clear that genome sizes are correlatedwith neither the size nor the complexity of the different species. This seemingparadox is explained by the fact that the large eukaryotic genomes contain largeamounts of non-coding DNA. In humans, for instance, only about 1.5% of thegenomic DNA codes for protein products, and only about 28% of it is transcribedinto RNA. A large part of the remaining DNA is composed of highly repetitivesequences, which are often referred to as “junk-DNA.” However, the non-codingDNA is not all insignificant, because some of those sequences have importantfunctions as structural elements of the DNA or have contributed (or may contributein the future) to the evolution of the genome.Although the cellular genomes are very large, they function in very controlled

manner. Among all the multiple genes, and in the middle of the very large non-coding sequences, the functional genes are expressed in a highly coordinatedfashion: the amount, timing, and location of the expression of each gene areaccurately regulated. The gene regulation is mediated mostly by different proteins– but in many cases also by small, non-coding RNAs.Different proteins, RNAs, membranes, and small soluble molecules such as

sugars and salts fill up the cellular contents, up to a level of molecular crowding in

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the interior space. Although the cellular contents are very complex, their centralfunctions are uniform between all different cells and between all species. Partic-ularly, the genetic code itself and its expression mechanism are the same, inprinciple, in all species (Fig. 4.5).

4.2.2.2 The Genetic Code and Its ExpressionThe genetic information is encoded in the nucleotide sequences in groups ofthree adjacent nucleotides, the codons, each corresponding to specific aminoacids (or a stop sign). Although the four nucleotides (A, G, C, and T in DNA;in RNA, T is replaced by U) can be organized into a total of 43 = 64 different tripletcombinations, only 20 different amino acids are utilized and coded for in thecurrent life forms – although some prokaryotes use 22 different amino acids.Thus, the coding system includes some redundancy: several codons code for thesame amino acid (Table 4.2). Each gene is composed of a set of triplet codons. Thecode of each gene (or the open reading frame, ORF) starts at a specific ATG tripletin the DNA and continues until it reaches one of the following triplets: TAG,TAA, or TGA, which do not code for any amino acid. These stop codons mark theend of the gene (Table 4.2). In eukaryotes the genes are often interrupted byintervening sequences (introns) that must be removed from the sequence duringits expression process.

4 From Molecular Evolution to Cellular Life94

Fig. 4.5 Flow chart of the expression of genetic information.

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4.2 Life as It Is Known 95

Table4.2

Thegene

ticcode

,com

posedof

triplets

ofthefour

nucleicacid

basesuracil(U

),cytosine

(C),ad

enine(A),

andgu

anine(G

),an

dtheirinform

ation(aminoacid

orstartor

stop

codo

n).

Firstbase

Cod

onSecond

base

UInform

ation

Cod

onSecond

base

CInform

ation

Cod

onSecond

base

AInform

ation

Cod

onSecond

base

GInform

ation

Thirdbase

U U U U

UUU

UUC

UUA

UUG

Phen

ylalan

ine

Phen

ylalan

ine

Leucine

Leucine

UCU

UCC

UCA

UCG

Serine

Serine

Serine

Serine

UAU

UAC

UAA

UAG

Tyrosine

Tyrosine

Stopcodo

nStopcodo

n

UGU

UGC

UGA

UGG

Cysteine

Cysteine

Stopcodo

nTryptop

han

U C A G

C C C C

CUU

CUC

CUA

CUG

Leucine

Leucine

Leucine

Leucine

CCU

CCC

CCA

CCG

Prolin

eProlin

eProlin

eProlin

e

CAU

CAC

CAA

CAG

Histidine

Histidine

Glutamine

Glutamine

CGU

CGC

CGA

CGG

Arginine

Arginine

Arginine

Arginine

U C A G

A A A A

AUU

AUC

AUA

AUG

Isoleu

cine

Isoleu

cine

Isoleu

cine

Methionine,

startcodo

n

ACU

ACC

ACA

ACG

Threon

ine

Threon

ine

Threon

ine

Threon

ine

AAU

AAC

AAA

AAG

Asparagine

Asparagine

Lysine

Lysine

AGU

AGC

AGA

AGG

Serine

Serine

Serine

Serine

U C A G

G G G G

GUU

GUC

GUA

GUG

Valine

Valine

Valine

Valine

GCU

GCC

GCA

GCG

Alanine

Alanine

Alanine

Alanine

GAU

GAC

GAA

GAG

Asparticacid

Asparticacid

Glutamic

acid

Glutamic

acid

GGU

GGC

GGA

GGG

Glycine

Glycine

Glycine

Glycine

U C A G

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The genetic code is interpreted (or expressed) in a multi-step process (Fig. 4.5) thatconverts the sequence of the nucleotide triplets into a linear sequence of thecorresponding amino acids (Table 4.2). First, the sequence of the target gene iscopied (transcribed) into a messenger RNA (mRNA). The mRNA contains thesame sequence as the corresponding DNA, but in contrast to DNA, the RNApolymer is short-lived and is used only for short-term expression of the code.The mRNA associates with the two subunits of the ribosome, which then movesalong the mRNA and recognizes the triplet code, starting from the first AUG codonon the mRNA (corresponds to the ATG on the DNA). The nucleotide triplets arerecognized by the anticodon triplets of the aminoacylated transfer RNAs (tRNAs),which enter into the ribosome complex and bring in the specific amino acidscorresponding to each triplet codon. The peptide bonds between the adjacentamino acids are formed by the catalytic RNA component of the ribosome (riboso-mal RNA, rRNA). As these amino acids are brought into the reaction complex, theribosome joins them into a long chain or “translates” the nucleotide sequence intoan amino acid sequence (Fig. 4.5). The produced amino acid chain is initially calleda polypeptide, but after it folds into the accurate three-dimensional structure, itbecomes a functional protein.Thus, the components needed for the expression of the genetic code are the

mRNA, the tRNAs and the amino acids, and the ribosomes. The ribosome itself iscomposed of multiple proteins and RNAs (varying from 52 to 79 proteins and fromthree to four RNAs in different species). Each of the steps of the gene expression(transcription, tRNA amino acylation, and the translation itself) requires multipleaccessory proteins for correct function and regulation. This strong protein depend-ency of the whole gene expression process creates a dilemma similar to the one ofthe chicken and egg. Proteins are required for expression of the genetic code as wellas for the maintenance (or replication) of the code, and the code is needed for theexpression of the proteins. Thus, how could the genetic DNA first be generated andreplicated, and how was its expression machinery first established – how did thiscyclic process get started?It is assumed that the storage and expression of the genetic information were the

first hallmarks for life as we know it and that these were the key elements in themolecular evolution that led to the birth of the LUCA. They existed already at thetime of the LUCA, and they required functions such as genome replication,transcription and translation, and pathways for amino acid and nucleotide syn-thesis. These functions are so essential for present life that their origin is thecentral part of the question of the origin of life as a whole.

4.3Last Universal Common Ancestor (LUCA)

The features that occur in all life forms are essential to life. Therefore, they shouldhave been present already in the earliest established cellular life, i.e., in the LUCA.Such conserved features include

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• the enclosure or containment in cell membranes,• the genetic code, and• the translation machinery for the expression of the code

(the ribosomes, tRNAs, and amino acids).

Some enzymes related to RNA and amino acid biosynthesis and degradation and toenergy production and use (cell metabolism) also are common to all cellular life. Afurther curious detail that is fully conserved in all cellular life is the symmetrybreaking, or homochirality, occurring in its central molecules: all the amino acidsused in the cellular proteins are of the same stereoisomer type, which is the left-handed (L)-configuration (see Chapter 2), and the deoxyribose and ribose sugarsused in all the nucleotides are of the right-handed (D)-configuration only, meaningthat the bond between the carbons in positions 4 and 5 points up, not down(Fig. 4.4).

4.3.1Containment in a Cell Membrane

As mentioned earlier, all life on Earth is cellular, which means that it is allcontained within, and separated from its environment by cell membranes. Thiscontainment is important for many reasons. Themolecules synthesized in the cellsdo not escape into the environment, and the concentrations of the intracellularmolecules are maintained at desired levels by regulating their synthesis anddegradation. Molecules from outside are transported in and out in a regulatedmanner, and the cellular molecules interact and function in amutually coordinatedway. Further, because the cell membrane physically connects the genomes withtheir respective gene products, the selection for beneficial products and functionsbecomes targeted to their corresponding coding sequences, i.e., the genes canevolve based on their products. The physical connection also allows the jointmaintenance of different segments of the genomes and allows their coevolutiontowards synergistic functions. All in all, the cell membrane allows all cellularcomponents to function and evolve as one coordinated entity and unit.The excellent utility of present-day membranes is related to their highly

sophisticated properties. Cell membranes are formed of amphiphilic (i.e., oneend is hydrophobic and the other end is hydrophilic) molecules called lipids,which aggregate in water and assemble into bilayers (see Chapter 3). These lipidbilayers are themselves impermeable to water, but they are spanned by severaldifferent proteins that serve as transport channels for water-soluble moleculesand as receptors for external signals and cues. The cells may also adjust theproperties of their membranes by changing their protein components or bychanging the saturation level of lipids according to temperature. Cells continu-ously produce new lipids for the growth of their membranes, and different lipidsare produced to construct membranes for different compartments. Thus, mem-branes in current cells are very dynamic and functional. However, the situationwas quite different at the time prior to the existence of the proteins needed for

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lipid biosynthesis or for membrane transport channels. How could the cells becontained at this stage?It is possible that some type of membrane was formed in the early world by

spontaneous assembly of abiotically formed lipids. It has been shown that differentpolar hydrocarbon derivatives, containing 10 or more carbons in their hydrocarbonchain, are amphiphilic molecules that may assemble into bilayers, and these againmay spontaneously form vesicles in aqueous environments. Such aliphatic (or linear)and aromatic (or circular) hydrocarbons are present, for instance, in the carbonaceouschondrites (see Chapter 3). Hydrocarbon–lipid vesicles might have enclosed theearliest genomes and functioned as compartments for their replication. However,this scenario involves severe problems. Because the hydrophobic lipid membranesseparate the organism from the surroundings, they may prevent access to theirresources, such as useful molecules available in the surrounding. Further, becausethe organism is closed inside a “dead” membrane, it may not be able to expand ordivide or to allow its progeny to accumulate beyond its own original compartment.Several membrane chemists, e.g. the research groups of Deamer, Luisi, and

Szostak, have attempted to resolve the assembly and the functional parameters ofspontaneously assembled membrane vesicles. They have shown that the perme-ability of the bilayer membranes is related to the length of the aliphatic carbonchains: modified hydrocarbons of less than 14 carbons are permeable for smallionic molecules, such as amino acids and phosphates. Actually, lipid membranesformed of carbon chains of less than 10 carbons are too permeable to maintain anyion gradient. The membrane vesicles formed of longer fatty acids, such as oleicacid, are semipermeable: small molecules, such as nucleotides or amino acids, maydiffuse through them while large polymers may not. This property would allowspontaneous uptake of nucleotides into the vesicles and retention of the polymersinside them. This process would increase the osmotic potential inside of thevesicles and cause the growth of the membrane via incorporation of more fattyacids drawn from emptier vesicles or frommicelles. Thus, themere hydrophobicityof fatty acids or of other lipid molecules may have caused the prebiotic assemblyand function of primitive, cell-like structures. Indeed, assembly and growth, andeven division of such lipid vesicles, have been demonstrated in laboratory con-ditions. Likewise, nucleotide and amino acid polymerization inside the vesicle hasbeen induced, simulating the assembly of small, artificial cells.To have an adequate supply of the lipids (or of amphiphilic carbon chains) for

membrane assembly, the LUCA would have needed the pathways to synthesizecarbon chains containing at least 10 carbons. A significant dilemma related to theorigin of the lipid biosynthesis pathways is that in present life two completelydifferent types of lipids are used for cell membranes: the Archaea use isoprenoid-type carbon chains (polyunsaturated hydrocarbons with methyl side chains), andthe Bacteria and Eukarya use fatty acid–type (unbranched) carbon chains. Thesetypes of carbon chains are produced via completely different pathways, and thepathway utilized in Archaea does not even exist in Eukarya or in Bacteria. Thus, it isdifficult to deduce what kind of lipid biosynthesis might have been utilized in theLUCA and how this early membrane synthesis gave rise to two different mem-

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brane compositions. It is possible either that several different lipid biosynthesispathways were established in the LUCA population, or that the cellular membranesynthesis pathways were established after the divergence of the three domains.However, this latter scenario would leave open the question of how, or in what, theLUCA was contained.It has been suggested by some geochemists that prebiotic reactions and early life

would have utilized some other types of compartments, formed of inorganic surfa-ces. W�chtersh�user (2003) has proposed that prebiotic chemistry might haveoccurred on surfaces of clays or minerals where the earliest cells might then haveassembled. These minerals would have catalyzed the reactions and stabilized theforming polymers (see Chapter 1). Martin and Russell (2002), Koonin and Martin(2005), and Brown propose that the porous, chimney-like structures of metal sulfide(mainly FeS) precipitates, formed at the hydrothermal vents at the bottom of theearly ocean, functioned as chemically rich, protective hatcheries that providedcontainment and suitable chemical conditions for the chemical evolution towardslife. The main attractions of these latter ideas are as follows.

• Firstly, those metal sulfide mounts were formed from amultitude of small, interconnected compartments, whichmight have served as containments for chemicals and ascatalytic surfaces for reactions.

• Secondly, the hydrothermal vents produced a continuousflow of warm geothermal fluid, full of several different re-duced chemicals, and it maintained a strong reduction gra-dient between the H+-rich geothermal fluid and (supposedly)alkaline seawater, driving the reduction chemistry of themolecules.

• Thirdly, the hydrothermal vents produced a temperaturegradient, providing convection flows to cycle the macromo-lecules between double-stranded and single stages (discussedin Section 4.6).

The combination of all these factors might have allowed the evolution of complexmolecular communities in the cell-like inorganic compartments, until they wereadequately competent to produce lipids and proteins for cellular membranes andstructures and might escape from the hatchery to self-sustained life in the outsideworld.

4.3.2Genes and Their Expression

One experimental way to study what properties and functions were present in theLUCA is to look at which genes or sequences are still common to all the organismswhose sequences are known today (assumably derived from the common origin).Lazcano and coworkers compared a set of fully sequenced genomes and found 283genes that are highly conserved in all Eukarya genomes, 24 that are highly

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conserved in Bacteria, and 145 that are conserved in Archaea. In all domains thesegenes include putative ATPases (for conversion of proton gradients into adenosinetriphosphate [ATP] synthesis and for utilizing the energy of ATP), genes involvedin transcription and translation, as well as RNA helicase and enolase, phosphor-ibosyl pyrophosphate synthase, and thioredoxin genes, which are involved innucleotide biosynthesis and RNA degradation. Such genes, if they were presentin the LUCA, indicate that the organism possessed means for maintaining itsgenetic information (at least in RNA form) and a translation system. Because theATPases locate in the membranes and produce ATP (as energy compound) byutilizing proton gradients formed across the membranes, this indicates that LUCAhad a cell membrane and produced and used energy in the form of ATPmolecules.Another approach to model primitive life is to analyze what would be the

minimal set of genes required by the simplest cells today. Several groups ofbioinformatists have worked on such questions. Gill and coworkers have searchedthe genomes of the smallest existing cells (bacterial and archaeal species, whichlive as endoparasites inside their host cells) for the set of genes that seemmandatory for them all. The living environments of these species are chemicallyvery rich, and the cells may obtain a large part of all their required biochemicalprecursors from their hosts. Therefore, they have lost the corresponding genesfrom their own genomes and have evolved, by reduction, towards ultimately smallgenomes. Comparison of the genomes of such species revealed that they have 206genes in common. All species have additional genes that allow them to survive intheir specific environment (host), but these 206 genes seem to comprise theobligatory set of genetic information required in all these species. Thus, it canbe reasoned that a comparable set of genes is essential for any cellular life, evenwhen living in the most protected and nutrient-rich conditions. Thus, if the LUCAwas a well-established cellular species, sustained in its own (probably chemicallyrich, easy, and protected) environment, it probably had to possess at least thisnumber of gene different functions.As the early organisms evolved to more complex, the initial sequences were

converted via mutation and recombination to code for new functions. The genomesgrew larger by duplicating, recombining, and modifying what they already had:new genes were often produced from previously existing ones, by recombining andmodifying functional protein domains (3-dimensional structures). Recent proteinstructure analysis by Doolittle and coworkers has identified a set of 49 protein-folding domains (or folding super-families) that are present in all analyzed ge-nomes of the three domains of life, suggesting that these protein-folding structureswere already present in the LUCA. Again, these protein structures occur in theproteins related to translation and to metabolic and glycolytic enzymes.So far, it has been reasoned that LUCA was a fairly complex organism. But how

did it diversify into the three domains of life that we know today? The threedomains differ from each other in such ways that their direct descent from oneanother, in a fixed order, is difficult. Each pair of domains shares some featuresthat are lacking from the third domain (Fig. 4.6), so it seems that none of them isdirectly derived from the others.

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Because the deviation of the three domains from the LUCA is difficult to traceback, the question of the order of the establishment of the three domains remainsopen, i.e.:

• whether the prokaryotes differentiated as two branches fromthe LUCA and then formed the eukaryotes later by mutualfusion;

• whether the eukaryotes were derived directly from the LUCAand later gave rise to the prokaryotes (e.g., by plasmid escapeand reduction processes); or

• whether the three domains diverged separately from a mixedLUCA population.

When this question has been addressed by phylogenetic studies, different resultshave been obtained from different genes. For instance, the classical phylogenetictree based on 16S-rRNA sequences, first produced by Woese and coworkers in1990, shows the early deviation of the Bacteria and Archaea domains, with thethermophilic Bacteria and Archaea at the base of the different branches, and thelater deviation of the Eukarya domain from the Archaea (Fig. 4.7A). However, someauthors, e.g., Poole and Forterre, suggest that the phylogenetic analysis may notaccurately resolve the most ancient sequences: after very long (or very fast)evolution, sequences may become so saturated with mutations that they appearas more conserved in the phylogenetic analysis.When different protein gene sequences are analyzed, diverse phylogenetic trees

are produced for the different sequences. This may indicate that the domains havenot evolved as separate lines but rather that the genes have been mixed by stronglateral gene transfer after the separation of the domains.It is now widely discussed (see reviews by Pennisi and Doolittle) that the

intensive lateral gene transfer between species, and even between domains, mayhave mixed the initial lineages so effectively that it may be difficult to trace back anyoriginal sets of genes associated with the early phylogenetic lines. Such lateral genetransfer would have been possible because the newly separated lineages were stillvery simple, similar, flexible (nonspecific), and rudimentary in their functions.Therefore, they might utilize the same novel functions and structures, even if those

4.3 Last Universal Common Ancestor (LUCA) 101

Fig. 4.6 Distribution of some key conservedfeatures among the three domains of life: eachof them is shared by two domains only.

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were transferred across the domain borders. The DNA exchange could have beenmediated via cell fusions or via direct DNA uptake (gene transfer or cellularconjugation) – or via third parties, such as viruses or plasmids (gene transductionor transformation).Particularly in eukaryotes, the uptake of foreign (prokaryotic) DNA may happen

via eating up (endocytosis) of foreign cells. This process is still a distinct function of

4 From Molecular Evolution to Cellular Life102

Fig. 4.7 Phylogenetic lineage of the three domains of lifedetermined by different genetic sequences. (A) 16S ribosomalRNA sequence (adapted from Woese et al. 1990); (B) severaldifferent sequences (adapted from Doolittle 1999).

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some eukaryotic cells. Mitochondria and chloroplasts are well-known examples,indicating that endocytosis of other species has occurred in the history of differenteukaryotes. In these instances the engulfed prokaryotes were maintained intact inthe cytoplasm and established as beneficial endosymbionts, or organelles, of thecells. Considering the strong lateral gene transfer, the tree of life at its earlier stageslooks rather like a bush (Fig. 4.7B).

4.3.3Hypothetical Structure of the LUCA Genome

The dilemma of the differentiation of the three domains relates to the question of thetype and structure of the LUCA genome. It is commonly thought that LUCA shouldhave been similar to the simplest life forms existing today, the prokaryotes. Accord-ingly, it should have been driven by a small, circular DNA genome. However, Pooleand Forterre and their coworkers argue that the circular, supercoiled prokaryoticgenomes with a single origin of replicationmight represent a later adaptation to veryfast and efficient replication strategies.The most primitive DNA genomes may havebeen linear, like the RNA genomes (see Section 4.4), which are thought to havepreceded the DNA genomes. One argument supporting the idea that the eukaryote-like linear genome structure is themost original one is that specific catalytic RNAs –apparent relicts of the earlier RNA genomes – are still used to process different RNAproducts in the eukaryotes (Table 4.3), while many of them have been replaced bymore efficient (and advanced) protein catalysts in the prokaryotes. Likewise, tRNA-like components are still utilized in the enzymes (telomerases) that maintain thetermini (telomeres) of the linear eukaryote chromosomes, suggesting that theseterminal structures are derived from the genomes of RNA-based life.The primitive RNA genomes may have influenced the ploidy level (the copy

number) and the fragmentation (chromosome number) of the later-arriving DNAgenomes. The early RNA genomes were very fragile and prone to degradation, andthe inaccurate replication processes accumulated multiple mistakes in their se-quences. For these reasons, the genomic components did not grow very large. Inorder to accumulate more coding capacity, the genomes should have been com-posed of multiple short components. To avoid the loss of genetic information dueto high mutation rates, the cells should have maintained more than one copy ofeach genomic component, and thus diploid (or maybe multiploid) rather thanhaploid (prokaryote-like) genomes should have been used (although one has tobear in mind that prokaryotes also normally maintain several copies of theirgenome in each cell). The earlier RNA-genome strategy may have been maintainedafter conversion to the DNA form, suggesting that the earliest cellular genomesshould have been composed of multiple, short, linear components, each presentedin more than a single copy.It is not clear whether the LUCA had evolved, as yet, to the DNA stage, or

whether the transition from RNA to DNA genomes occurred separately in the threedifferent lineages after their separation from the LUCA. Later conversion fromRNA to DNA genomes may be supported by the fact that different types of DNA

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4 From Molecular Evolution to Cellular Life104

Table4.3

Exam

ples

ofpresen

t-da

yRNAcatalystsan

dotherfunction

alRNAs.

RNA

Function

Distribution

Putative

occurren

cein

theRNA

orRNPworld

Ribosom

alRNAs

Translation:structuralan

dcatalytic

Ubiqu

itou

sYes

mRNAs

Carriersof

thegenetic

code

Ubiqu

itou

sYes

tRNAs

Translation:A

minoacid

tran

sport

Ubiqu

itou

sYes

tRNA

Aminoacid

metabolism

Ubiqu

itou

sYes

tRNA

Replicationprim

erRetrotran

sposon

s,retroviruses,

pararetroviruses

Possibly

Telom

eraseRNA

tRNA-like

prim

erforchromosom

een

dsynthesis

Eukaryotes

Yes

RNaseP

tRNAmaturation

Ubiqu

itou

sYes

snoR

NAs

rRNAprocessing

Eukaryotes,som

eArchaea

Yes

RNaseM

RP

rRNAprocessing

Eukaryotes

Related

toRnaseP

GroupIself-splicingintron

smRNAsplicing

Eukaryotes,som

eProkaryotes

Possibly

GroupII

self-splicingintron

smRNAsplicing

Eukaryotes,som

eProkaryotes

Possibly

srpR

NA

Protein

tran

slocation

Eukaryotes,som

eArchaea

Yes

vaultRNA

Not

know

n–Protein

tran

slocation?

Eukaryotes

Possibly

G8RNA

Maintenan

ceof

ribo

somal

apparatus

atelevated

temperatures

Eukaryotes

Probably

Ham

merheadan

dhairpin

ribo

-zymes

Self-cleavage

andlig

ation

Viroids

andsatRNAs

Probably

Sou

rce:Mod

ifiedfrom

Jeffares

etal.1

998.

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polymerases are utilized by Bacteria and by Archaea and Eukarya. Also, if the RNAgenomes were stabilized via methylation of the 2’ hydroxyl groups of the ribosemolecules, as suggested by Poole, it is conceivable that the RNA genomes mighthave developed to be fairly large, gaining significant coding capacity. Such RNAgenomes may have been adequate to support self-sustained cellular life and toproduce codes for the ribonucleotide reductases, thymidylate synthases, and re-verse transcription enzymes eventually needed to convert the ribonucleotides intodeoxyribonucleotides and RNA sequences into DNA. Forterre suggests that thoseDNA-producing enzymes and, consequently, DNA genomes were invented severaltimes to establish DNA-based viral genomes colonizing the RNA cells and that theywere transferred from those to the RNA-based host cells, in three separate transferevents, to establish the three DNA-based domains of life.Woese has suggested that at the earliest stage of evolution, when the genomes

were still very small and unstable, the fully functional genetic information couldnot exist in individual discrete organisms or genomes. He suggests that these earlygenomes instead formed a diverse community of organisms that dynamicallyinteracted with each other, exchanging, testing, storing, and evolving alternativegenomic sequences. Woese calls these early life forms “progenotes,” which de-scribes the evolutionary stage preceding the fixed genomic life forms, or the“genotes.” Again, it is not clear whether such progenotes would have had a DNAor an RNA genome; maybe they could have been characteristic both before andafter the transition from RNA to DNA genomes.

4.4“Life” in the RNA–Protein World: Issues and Possible Solutions

LUCA appears to have been a fairly complex and well-established organism – butfrom where did this complexity arise? Information flow from DNA into mRNA andthen into proteins (Fig. 4.5) demands multiple functions in between; therefore, it iscommonly thought that the whole genetic machinery had to evolve from a simplersystem. It is supposed that the genetic system preceding the DNA genomes wereRNA genomes, which could have functioned as information storage media and astemplates for translation. It is thought that the protein synthesis became estab-lished at the time of the RNA genomes and that the appearance of the proteincatalysts then allowed the “invention” and establishment of the DNA genomes.Thus, present-day DNA–RNA–protein life would have been preceded by lifecomposed of RNAs and their encoded protein products – or by RNA–protein(RNP) life.At the earliest stages, when the genetic code was translated into protein products,

or the genetically encoded proteins were “invented,” both the codes and theirexpression system were certainly very primitive. The codes had not yet evolved tocode for specific functions, and also the translation system was very inaccurate.Maybe only a few of the currently known amino acids were used. The system wasable to produce only a few short, nearly random polypeptides. The polypeptides had

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not been adapted to specific functions, but maybe some of them could bind to RNAand function as scaffolding or structural proteins, similar to present-day chaper-ones. Such structural proteins may still have been quite useful in stabilizing theRNA genomes and in holding them in suitable three-dimensional structures toenhance their catalytic properties. Such structural proteins probably assisted in themost essential functions of the RNP world, i.e., in the replication of the RNAs. Thehigh mutation rate produced more functional gene products, and in due coursesome proteins appeared that actually catalyzed the replication of RNA genomes.

4.4.1Evolutionary Solutions

The early enzymes were still very inefficient and prone to errors. Therefore, eachtime the genomes were replicated, considerable portions of the nucleotides werecopied wrong and the genetic information was altered. If the sequences mutatedtoo much, it was changed into a non-functional form, the gene was no longermaintained, and the information was totally lost. This critical level of accumulationof errors has been defined by Manfred Eigen as the “error threshold” and is nowknown as the “Eigen limit.” The number of incorrectly copied nucleotides in-creased with the genome length; the longer the genomes, the easier they accumu-lated fatal levels of mistakes. Thus, only fairly short genomes (or genomic compo-nents) could be maintained by this very error-prone replication.Eigen has demonstrated how the evolution of small genomes (e.g., viral ge-

nomes) functions in a cyclic fashion, where repeated improvements of differentsynergistic functions lead to very efficient improvement of fitness and adaptationto new conditions. As described by Poole, this cyclic adaptation and genome-building model seems applicable for the gradual improvement of the RNP organ-isms: the new sequence variants encoded for improved replicase proteins or newcomponents for the translation machinery. These produced better replicase mol-ecules and thereby improved the accuracy of the replication. This again allowed themaintenance of longer genomes – and the increasing coding capacity allowed forthe production of new components for the replication and translation machineries.

4 From Molecular Evolution to Cellular Life106

Fig. 4.8 Darwin–Eigen cycle demonstratingthat Darwinian selection for improved repli-cation and translation allowed maintenanceof larger genomes, and these again allowedfor improved replication and gene expression.Thus, the increasing genome size, new genefunctions, and improving replication andtranslation fidelity have mutually enhancingeffects on the evolution of complexity (adaptedfrom Poole et al. 1999).

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Thus, Darwinian selection for more accurate replication and the correspondingincrease of the genome size (determined by the Eigen limit) together enhanced theevolution towards more complex genomes (Fig. 4.8).

4.4.2Solutions Found in the Viral World

It is of interest that present-day single-stranded (ss) RNA viruses possess multiplefeatures that seem similar to the properties of a hypothetical early RNP organisms.As in the RNP organisms, the viral genomes are composed of short linear RNAsthat code only for a few necessary gene products. The total length of RNA virusgenomes seems to be limited by both the fragility of the RNAs and the Eigen limit(the avoidance of accumulating too many errors by inaccurate replication); thus, atthe present time the longest ss RNA virus genomes – those of the coronaviruses –contain about 30 000 nucleotides. The smallest viral genomes, – those of theleviviruses – are only about 3 500 nucleotides long and code only for three proteins,namely, the replicase protein, the coat protein, and a maturase protein to interactwith the host. These seem to make the minimal protein set required for sustainableviral genomes. In many viruses the replicase proteins are divided in two separatecomponents, the helicase and the replicase, apparently because those proteins needto be produced in very different amounts.The coat protein is required to enclose the RNA and to protect it from degrada-

tion. All viruses encode one or more of other gene products to interact with theirhost cells – mainly in order to suppress the host defense functions – but it appearsthat in principle the replication and the protective functions are the most importantrequirements for viral survival. This may also indicate how important theseproteins may have been to the early RNA replicators.Viruses maximize the use of their limited genomic sequences – they use them in

the most efficient way. They contain a minimal amount of non-coding sequences,and they do not “invest” any coding capacity for producing regulatory proteins,which are so essential for cellular life. Many viruses regulate their essentialfunctions – initiation of replication and translation – by short and simple sequen-ces at the termini of the RNA genomes and by interactions between RNA loops andsequences. With such RNA interactions, some viruses are capable of dedicatingtheir genomic RNAs to function in either the replication or the translation mode,which avoids collision of the two opposite processes.Being parasites of the cellular world, RNA viruses make their living in a chemi-

cally rich environment: the host cells provide all the building blocks of the macro-molecules (the nucleotides and the amino acids) and the translation machinery foruse by the viruses. Likewise, the early RNP organisms had to live in a similarenvironment, because they had no means for synthesizing their own buildingblocks. Through their evolutionary history, the RNA viruses have become veryefficient in their replication and in their adaptation to their own specific hostorganisms. Indeed, in spite of their ultimately minimal size, the RNA viruses arevery successful. There are many more species of viruses than there are cellular

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species, and each cellular species may be infected by several different viral species.It is possible that the (fully evolved) RNP-based life forms were efficient andsuccessful replicators. Apparently they had to be quite advanced in order toproduce adequately large genomic pools to give rise to DNA-based life and cellularorganisms. Some of the early RNP-based replicators may have survived to form thebase for the massive variation of present-day viruses.

4.5“Life” Before the Appearance of the Progenote

4.5.1The Breakthrough Organism and the RNA–Protein World

The first protein-mediated functions initiated evolution towards more and morecomplex biochemistry. Therefore, the initiation of genetically encoded proteinsynthesis has been the key step in the development of any more-advanced life.This event has been considered so essential that Poole and coworkers have namedthe first creature that produced proteins the “breakthrough organism.” But howcould this hypothetical breakthrough organism break through – or, how might ithave come into existence in the first place?Clearly, it had to evolve from simpler systems through a cascade of improving

stages. It was required that it be able to synthesize mRNA-like translatablesequences and to run a primitive translation machinery consisting of ribosomes,tRNAs, and amino acids. Because protein synthesis did not exist prior to this time,the assembly or function of this primitive translation machinery could not havedepended on any specific proteins. Thus, the early translation reactions had to becatalyzed by the existing RNAs alone. This is theoretically feasible because in all thepresent-day life forms, the formation of the peptide bonds between amino acids isspecifically mediated by one RNA component of the ribosomes. Different naturalor in vitro–selected RNA molecules may catalyze many other reactions (for thenatural ribozymes, see Table 4.3). For instance, ribozymes have been found thatcan mediate the amino acylation of tRNAs. Thus, according to experimental data, itmay be postulated that mere RNA components were able to mediate the earliesttranslation process.

4.5.2Primitive Translation Machinery

A logical requirement for the existence of RNA-based translation machinery is thatthis machinery itself was initially generated and maintained in a protein-independ-ent manner. Present-day ribosomes are massive complexes, containing either three(in prokaryotes) or four (in eukaryotes) RNAs that vary in size from 120 to 2 904nucleotides. The genes coding for these RNAs take, together with their interveningsequences, more than 7 500 nucleotides of genomic sequences. It is clear that the

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earliest RNA components were not as long as they are today. As mentioned inSection 4.4.1, the error-prone replication systems produced only fairly short RNAstrands that are estimated not to have exceeded a few hundred nucleotides in length.Thus, it is likely that the proto-ribosome had to be composed of short fragments ofRNA that jointly formed one functional complex. This may still be evident inpresent-day ribosomes, because their interaction with tRNAs may be mimicked bya separate small RNA analogue of the ribosomal RNA sequence and because peptidebond formation is catalyzed by a specific adenine in the core of the ribosomal RNA.Thus, it seems likely that the present-day ribosomal RNAs (rRNAs) developed via acombination of previously existing, small functional subunits.

4.5.3Origin of Ribosomes

Even if the early ribosomes were formed of small separate RNAs, their mainte-nance required that they be reproduced fairly accurately. The mere existence ofsuch a functional complex required that it had evolved gradually from somesimpler structures – which again had been maintained and selected for their

4.5 “Life” Before the Appearance of the Progenote 109

Fig. 4.9 Model of the early function of the proto-translationmachinery as RNA replication complex (from Poole et al. 1998,with permission from the publisher).

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preexisting function(s). The most important function at this stage would have beenthe maintenance of the existing sequences, namely, the replication of RNAs. Pooleand coworkers have proposed that the original function of the proto-ribosomalcomplex was the replication of RNAs. According to their model, the early proto-ribosomes extended the complementary RNA strand on the RNA template byligating nucleotide triplets (corresponding to present-day anticodon loops) broughtinto the reaction by tRNAmolecules or their primitive precursors. This means thatearly replication was mediated by ligation rather than by polymerization. Incorpo-ration of nucleotide triplets rather than single nucleotides had the advantage ofallowing higher affinity and longer-lasting annealing of the incoming nucleotidesto the template. This allowed more time for the very slow RNA catalyst to performthe ligation (Fig. 4.9).According to this model, it is conceivable that amino acid acylation of the incom-

ing tRNAs was a significant step in the early replication process. The covalentbinding of the amino acids to the -CCA terminus of the tRNAs might have chargedthese molecules with energy, which might have been released by the detachment ofthe amino acid during the polymerization. This process might have been used todrive the polymerization. On the other hand, it is conceivable that the positivelycharged amino acids allowed the proper confirmation (tight folding) of the primitive(negatively charged) tRNAs and/or allowed their binding to the replicase complex.Release of the amino acids from the tRNAs might then have caused a conforma-tional change allowing for the release of the used tRNA from the complex.In any of these scenarios, the interaction between template RNA, ribosome, the

“triplet-reading” anticodons of the tRNAs, and the amino acids would have alreadybeen established at the early RNA replication function, prior to the invention ofprotein synthesis. Peptide bond formation might have been initiated as a sponta-neous reaction between the amino acids brought to close proximity by the incom-ing tRNAs. However, later conversion of the whole replication machinery into atranslation function is difficult to conceive – many things would be have beenrequired to change. For example, the hypothetic cleavage and ligation of thenucleotide triplets from the tRNAs and into the growing chain of RNA neededto be stopped and replaced by peptide bond formation. However, it is conceivablethat the introduction of protein synthesis made these changes possible, as itprovided protein catalysts for replication and a strong selection for the use ofribosomes for translation. Both processes, translation and replication, had to bemade to function on the same template in opposite directions. The function of thesame template in both replication and translation seems not to be a major obstacle,as it occurs in all present-day viruses in a coordinated and regulated fashion.Another model for the early role of tRNAs proposed byWeiner andMaizels is the

terminal taging of the replicating RNAs. These terminal tags would have func-tioned as the selective binding and initiation site of the replicase and thereby wouldhave helped to replicate the genomic ends correctly. This hypothesis is supportedby the fact that many present-day viruses have tRNA-like 3’ termini and thetelomerase enzyme that synthesizes the ends of the eukaryotic chromosomesfunctions on a tRNA-like template.

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4.6The RNA World

Logically, it is necessary to assume that prior to the invention of protein synthesis,all reactions required for maintenance of macromolecules – and for their evolutiontowards life – had to be mediated by molecules other than proteins. Present-dayRNA chemistry has demonstrated that different RNA molecules (either naturalones or selected in vitro) may mediate several different catalytic activities, althoughthe RNA catalysts typically function less efficiently than protein enzymes, i.e., at amuch slower rate (Fig. 4.2). Such molecules are called RNA enzymes or ribozymes.Most of the naturally occurring ribozymes mediate cleavage and ligation reactionsof their target RNAs (Table 4.3). The smallest ribozymes contain about 50 nucleo-tides and occur in the RNAs of viroids and viral satellite RNAs, while complexribozymes capable of many different catalytic functions can be artificially producedby in vitro selection.It must be emphasized that the functionality of the RNA catalysts is based on the

sequence information. The information does not code for any protein products, butit dictates the folding of the RNA into secondary structures that can recognize theirsubstrates and cause the desired reactions. Figure 4.10 shows the three-dimen-sional folding structure, the so-called hammerhead structure, of the smallestnatural ribozymes, which are composed of about 50 nucleotides.Figure 4.11 gives an example of the evolution of an RNA polymerase ribozyme,

as mediated by in vitro selection steps. The class I ligase ribozyme catalyzes thejoining of the 3’ end of an RNA strand to the 5’ end of the ribozyme (Fig. 4.11 a);the class II ligase ribozyme catalyzes the addition of three nucleotide 5’ triphos-phates (NTPs) to the 3’ end of the primer, directed by an internal template

4.6 The RNA World 111

Fig. 4.10 Three-dimensional folding structure(so-called hammerhead structure) of the small-est natural ribozymes. These self-cleaving and-ligating structures occur in several viroid andviral satellite RNAs and are composed of about50 nucleotides.

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(Fig. 4.11 b); finally, the class I–derived polymerase catalyzes the addition of up to14 NTPs on an external RNA template (Fig. 4.11 c).The hypothetic stage of early evolution, when all biochemistry was mediated by

different RNA catalysts, is called the RNA world. Invention of genetically encodedproteins brought out the new, protein-based biochemistry that soon replaced RNA-mediated catalysis. A curious example of this transition to protein-mediatedfunctions is that still today some proteins functioning in the regulation of trans-lation – namely, some translation elongation factors – are folded into a secondarystructure similar to that of the tRNAs. Apparently, after the RNA genomesaccumulated adequate coding capacity, the protein enzymes were able to convertthe RNA genomes to DNA form. Being much more stable than the RNAs, thesecould evolve into much larger sizes and superior coding capacity.With these immense improvements in biochemical functions, the original RNA-

mediated biochemistry might have disappeared without leaving a trace. However,this did not happen, as we do still have some clear molecular relicts, or molecularfossils, that apparently have been conserved from the RNA era into present-day life.The most convincing molecular fossil from the RNA world is that the primarygenetic code is still translatable only from RNA sequence (DNA exists only as aninformation storage system, comparable to a hard disk, containing all the data butno running program for translating this information). Further, the translationreaction, or the formation of the peptide bond, is still mediated by one RNAcomponent of the ribosomes, and the tRNAs still bring the amino acids into thetranslation reaction. Several other small functional RNAs exist in present-day cells(Table 4.3) and also may be functional relicts from the early RNA era.As mentioned in Section 4.3, some of these RNA catalysts – particularly those

that function in the maturation of different RNAs, especially small nuclear RNAsand nucleolar RNAs – as well as RNA-containing telomerase enzymes still occur in

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Fig. 4.11 Evolution of an RNA polymeraseribozyme mediated by in vitro selection steps.(a) The class I ligase ribozyme catalyzes thejoining of the 3’ end of an RNA strand (openline) to the 5’ end of the ribozyme; (b) theclass II ligase catalyzes the addition of three

nucleotide 5’-triphosphates (NTPs) to the3’ end of the primer, directed by an internaltemplate; (c) the class I–derived polymerasecatalyzes the addition of up to 14 NTPs on anexternal RNA template (from Joyce 2002, withpermission from the publisher).

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the eukaryotic organisms (Table 4.3). This suggests that those (slow) RNA-medi-ated functions have been maintained in eukaryotes from the times of RNA-basedlife. In prokaryotes, many RNA-processing functions have been replaced by pro-tein-catalyzed functions, apparently due to their adaptation to faster replication andto more efficient RNA processing, particularly in hot environments. For thesereasons it might be thought that the eukaryotic genome type – although expandedto huge sizes and complex gene sets over time – would be of a more ancient typethan the small and sophisticated prokaryote genomes.

4.6.1Origin of the RNA World

4.6.1.1 Prebiotic Assembly of PolymersIn order to get the functional RNA world started, preexistence of RNA polymerswas required. These RNA polymers supposedly appeared by spontaneous assemblyor polymerization of nucleotide monomers. They had to accumulate to significantamounts, and be of considerable length and variation, to ensure that this randomcollection contained some (or even one) that had the potential of copying itself and,later, of copying even other RNAs.The prebiotic, i.e., spontaneous, polymerization of RNA nucleotides is difficult to

explain with known RNA chemistry, because nucleotide polymerization requiresenergy and does not happen easily (see Chapter 3). It has been intensively studied –e.g., in the laboratory of James Ferris – and in these optimized conditions,polymers of about 40–50 nucleotides were produced. Such polymerization resultshave been obtained by allowing activated nucleotides to react in aqueous solutionin the presence of clay minerals, which significantly enhanced the polymerization.The enhancement by clays is caused, assumedly, by their fine-layered structure,composed of mineral grains with di- and trivalent positive charges. Those cationicsurfaces bind and immobilize the negatively charged nucleotides, placing them insuitable positions to promote their reactions with each other. Further on, bindingto the clay surfaces significantly stabilizes the ready-made RNA polymers, whichotherwise would be very easily degraded by hydrolysis.The group of Deamer reports that another environment that promotes RNA

polymerization, although to a lesser extent than clays, is the eutectic (very cold) icesolutions; an icy environment is also known to promote the ribozyme-catalyzedligation of RNAs. The liquid water phase remaining in between ice crystalsconcentrates the precursors effectively, and the low temperatures help to slowdown the reacting components to allow the formation of the phosphodiester bondsbetween nucleotides.For building the nucleotide polymers, the nucleotides need to be linked to each

other via phosphodiester bond between the 3’ and 5’ carbons of the adjacent sugars(Fig. 4.3). For this, the nucleosides first have to be phosphorylated at their5’ carbon. In the early world this was problematic because soluble phosphateswere not readily available. It is possible that the inorganic phosphate dissolved inlow amounts from calcium phosphate (hydroxyapatite) mineral or from volcani-

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cally produced linear polyphosphates, or from their breakdown products, andphosphorylated nucleosides to nucleotides. But this reaction is difficult and mightoccur only in the presence of urea, ammonium chloride, and heat.Polymerization of the nucleotides requires that they be activated by some high-

energy bond at the 5’ position to provide energy for the uphill reaction. In present-day life, this binding energy is obtained from the hydrolysis of the triphosphatemoiety, but this was not adequate in the prebiotic world because triphosphatesalone do not promote (non-enzymatic or non-catalyzed) polymerization. Therefore,it seems that the nucleotides had to be charged with other available molecules, suchas amino acids, bound with high-energy bonds at the 5’ position of the phosphory-lated nucleotides. The most effective activating groups, now commonly used forthe polymerization experiments in laboratories, are the different phosphorami-dates, such as phophoramidazoles. These compounds are formed from nucleoside5’ polyphosphates and amines or imidazoles; but such complex activating groupsmight not have been available in the prebiotic environment.A further complication in the polymerization of ribonucleotides is that in a

mixture of monomers, several different reactions take place. To make a functionalpolymer, the monomers must form the mono-phosphodiester linkage exactlybetween the 3’ and 5’ carbons of the adjacent nucleotides. However, the ribosering has reactive groups in carbons at positions 5’, 3’, and 2’ (Fig. 4.3). In prebioticconditions all these groups could react with each other, and cyclic compoundscould be formed between the 2’ and 3’ OH groups. Furthermore, the phosphatemolecules might have formed different polyphosphate linkages between differentcarbons. All these varying bonds would have produced dead-end products forfurther polymerization. It is still unclear what kind of conditions promoted thenucleotides to react in an orderly fashion to produce only the correct, 3’-to-5’-linkedRNA polymers (Fig. 4.4).

4.6.1.2 The Building Blocks of the RNA WorldFor synthesis of nucleosides, the purine bases adenine and guanine (A and G), thepyrimidine bases cytosine and uracil (C and U), and the D-isoform of cyclic ribosesugar are needed. Prebiotic synthesis and assembly of these nucleoside buildingblocks have been intensively studied by groups of chemists led by Gerald Joyce,Stanley Miller, Leslie Orgel, and Alan Schwartz. The prebiotic synthesis of thesecomponents, as well as the prebiotic synthesis of their small organic precursorssuch as CH4, NH3, CH2O, CNH, CN2H4, C3NH, CH2O, CN2H4O, and SH2, iscovered in Chapter 3.Provided that ribose sugar and the nucleobases were available, further on the

bases had to be covalently linked in �-orientation with the 1’ carbon of ribose toform nucleosides. This reaction may be activated by heating and it produces purinenucleosides, although with very low yield. Routes for prebiotic synthesis of pyr-imidine nucleosides are not well known, but they may be feasible via multiplesugar phosphate intermediates. Recently, a completely different route has beenfound, where Æ-D-cytosine was produced directly from ribose sugar and hydrogen

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cyanide. This efficient reaction thus produced cytosine, even if of the wrongisoform, and it also converted the existing (unstable) ribose into a stable form.Prebiotic synthesis of nucleotides would have yielded a racemic mixture of a

variety of different nucleotide analogues, both in Æ and � and in L- and D-isoforms.A spontaneous polymerization reaction of such (randomly) phosphorylated nu-cleotides would have been very slow and would have led to a wide variety ofdifferent linkages, formed between the whole variety of different nucleotide ana-logues and isoforms. Such randomly linked oligomers or polymers would not havebeen extendable or functional as templates for replication.Altogether, prebiotic formation of RNA nucleotides and their polymers, starting

from small molecular precursors such as HCN, NH3, CH2O, CH4, PO43–, or H2O,

involves so many unlikely or adverse chemical steps that many chemists havespeculated that RNA synthesis had to be preceded by simpler chemical polymers –or by nucleic acid analogues whose backbone is composed of non-chiral structures.Polymers proposed as hypothetical predecessors of the RNA world include peptidenucleic acids (PNAs) with a peptide as backbone, threose nucleic acids (TNAs), andpyranosyl-derived nucleic acids (p-RNAs) (see Chapter 1). If any of these polymerswas a direct precursor of present genetic material, then it must have been possibleto transfer the information by copying or transcription from this molecule intoRNA or DNA sequence, which indeed has been experimentally demonstrated forPNAs. However, the role of other polymers in the early steps of molecularevolution does not seem very plausible, because the central molecules of earlylife (the ribosomes and tRNAs) are based solely on RNA molecules.To find possible solutions for the appearance of the nucleotide-based (very

complex) genetic information, Cairn-Smith (1982) has postulated that instead oforganic polymers, entirely different molecules, such as minerals, may have con-tained the earliest pre-genetic (replicating) information. Still, it is not clear how anyspecific information would have been coded in the crystal structure of mineralsurfaces, or how these would have been converted to be biologically significant.Little is known, as yet, of what the available starting materials were, what theconditions were where the prebiotic chemistry took place, and what chemical andphysical reactions and selection processes were driving the increasing complexityof the early polymers (see also Chapter 1).

4.6.1.3 Where Could the RNA World Exist and Function?The question of the possible location and conditions of the proposed RNA world isvery difficult. It is assumed that the initial RNA polymers were formed by randompolymerization of nucleotides, but this scenario requires that the nucleotides hadto be initially available in the environment. Further on, for the synthesis ofnucleotides, their precursors – ribose sugar, purines and pyrimidines, and phos-phate molecules – had to be available. For the prebiotic synthesis of those com-pounds, their precursors or the small organic molecules such as CH2O, CNH,CN2H4, and HNCO had to be available in adequate amounts. To drive repeatedpolymerization reactions, leading to significant accumulation of the products

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(adequate for starting a whole new polymerization and replication network), a long-term, high-level supply of nucleotides would be required.The prebiotic synthesis or at least the accumulation of nucleotides would need to

happen in conditions where, further on, the nucleotides could spontaneouslypolymerize. The conditions also should have been adequately gentle to maintainthe polymers intact. The prebiotic synthesis of some of the precursors happenspreferably in cold or mildly warm conditions (synthesis of nucleic acid bases),while other steps require heat (nucleoside formation and phosphorylation). So it isconceivable that the locations for the different steps may have been temporally orlocally separate.The polymerization of nucleotides needs to take place in an aqueous environ-

ment because the nucleotides are water-soluble and liquid water is needed to carrythem into the reaction site. However, water efficiently reacts with the RNApolymers to hydrolyze the phosphodiester bonds, which breaks up the polymers.The hydrolysis reactions occur faster at higher temperatures; therefore, cool, closeto freezing temperatures would be more suitable for preserving RNA polymers.A further complication arises with the templated polymerization – meaning the

copying or replication of existing RNA strands. Because the phosphate groupsforming the phosphodiester bonds carry a negative charge of –1, the total chargeof the polymer is highly negative. In the templated replication, the complementarystrand is assembled on the existing template by hydrogen bonding between thecomplementary nucleotides (A to U andG to C) (Fig. 4.4). For stable assembly of thecomplementary strand, the negative charges of the phosphates need to be neutral-ized by an adequate level of soluble cations (positive ions). This neutralizationtogether with the hydrogen bonding of the bases leads to a stable assembly, andthe double-stranded product is closed for any further assembly of new strands on thesame templates. Thus, the double-stranded structure could be a dead-end product.To avoid this, some energy input or radical change of environment – e.g., by

dilution out of the cationic ions or warming up of the solution – would be needed toopen up the double helix. Lathe (2005) has proposed that alternating conditions oflow and high salt concentrations (as in tidal pools) would be needed to drive theassembly and separate the daughter strands. Brown and coworkers have experi-mentally shown that efficient melting (i.e., separation) of double-stranded nucleicacid strands can be obtained by convection-driven cycling of molecules in micro-compartments located in steep temperature gradients, such as the tiny compart-ments in the FeS precipitate mounts of hydrothermal vents.Still another putative environment that might have driven prebiotic chemistry

and the assembly of macromolecules, possibly including polymers, is the sandy orsilty beaches washed by the ocean tides. Bywater and Conde-Frieboes (2005) haveproposed that in these locations the ocean water would have brought in theprecursors for the reactions, and these might have been bound, by hydrogenbonding or ionic forces, to the cationic minerals in the clay and sand. Small dryingponds might have provided the concentration mechanism for the compounds, andthe subsurface layers of sand might have provided protection against UV radiation,as well as size-based fractionation and concentration by chromatographic filtration.

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The clay-like minerals would have been suitable catalytic surfaces for the assemblyof nucleotide polymers. The repeated washes by new waves or tides might haveprovided the cyclic dilution effects needed for the separation of the replicatingnucleotide strands, as proposed by Lathe.

4.7Beginning of Life

The above discussion should indicate that the origin of life was by no meanssimple. Rather, it should have been a procession through multiple stages ofspontaneous – but most often uphill – reactions of molecular chemistry andevolution towards cellular life. Within this procession it is difficult to determinewhen life actually started. It seems that there was a stage where the developingsystem was not yet clearly alive, and also no longer clearly lifeless, but swaying inbetween different directions of development in a type of bifurcating stage. Such athreshold level could have been achieved when the first sequences could replicatethemselves but when there were no biosynthesis pathways, as yet, for any of theprecursors or building blocks for making more of the same molecules. The systemwas modified and adapted by a selective evolution, but it was still wholly dependenton the supply of complex materials from its environment. It is conceivable thatsuch a threshold stage could have developed in several directions: one, for instance,to produce the semi-living (replicating but not autonomous) viral world andanother to produce autonomous cellular life. Parasitic and synergistic interactionsalso evolved – the viruses ending up as parasites of cellular life – but the earlymolecular interactions may have been more varied.The question of the beginning of life is related to how we define life. Life, as we

now know it, is very complex and versatile, but the definition should include justthe very minimal and first features that were required of a system to become alive.Andr� Brack has defined primitive life as an aqueous chemical system able totransfer its molecular information and to evolve (see Chapter 1). Eigen hasdescribed life as phenomena in the multidimensional information space, wherethe species – or quasi-species – form as their genomic sequences accumulate in theproximity of the optimal or best-adapted sequence, at so-called “fitness peaks.”Both these descriptions emphasize the information-driven nature of life, themaintenance of information via replication, and accumulation of new informationvia natural selection and evolution.In a reductionist way, it might be claimed that genomic information is the

essential part of life and that the cellular structure serves only as a vehicle tomaintain and renew the information. But the cellular structure has played a centralrole in the formation of information: the accumulated information just reflects theneeds of the cells, and the optimized information is determined by the adaptationof the cell to its environment.The very initial functional information appeared by accident, as a random

sequence was able to replicate itself. The further accumulation of information

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took place via improvement of that very function. When the system grew andevolved, new functions were “invented” that allowed the system to survive better inits environment. The selection, or genetic adaptation, was mediated via differentinteractions. Intracellular molecular interactions were, and still are, of essentialimportance, as were the interactions of the cell with its surroundings, with themembers of its own species, and with the whole surrounding ecosystem. Theseinteractions are the driving force for the accumulation of genetic information.Even the simplest cellular life is mediated via multiple biochemical reactions

driven by energy conversion reactions and, ultimately, by energy drawn from asuitable energy source. With these, life achieves a remarkable organization ofmatter and energy. The cellular structure is essential for the containment of allthese reactions and for the assembly of the organized structures.Thus, life is indeed based on genetic information and on evolution, but the third

essential party in the assembly of life is its cellular form. The cell and its inter-actions with the environment – and, on the other hand, its separation from theenvironment –build the entity that has allowed the accumulation of informationand that has facilitated evolution, and the self-sustained existence of the organism.Its existence still depends on suitable energy sources and availability of nutrients,i.e., on the life-supporting environment. A cell, adapting in its life-supportingenvironment, was the last defining requirement for the establishment of life aswe know it on Earth.

4.8Further Reading

4.8.1Books

Brack, A. The Molecular Origin of Life.Assembling Pieces of the Puzzle, CambridgeUniversity Press, Cambridge, 417 pp.,1998.

Cairn-Smith, A. G. Genetic Takeover and theMineral Origins of Life, Cambridge Univer-sity Press, Cambridge, 1982 (http://origin-oflife.net/cairns_smith/).

4 From Molecular Evolution to Cellular Life118

4.8.2Articles in Journals

Abe, Y. Physical state of the very early earth,Lithos 1993, 30, 223–235.

Berclaz, N., Muller, M., Walde, P., Luisi,P. L. Growth and transformation of vesiclesstudied by ferritin labeling and cryotrans-mission electron microscopy, J. Phys. Chem.2001, 105, 1056–1064. (http://www.plluisi.org/)

Biebricher, C. K., Eigen, M. The error thresh-old, Virus Res. 2005, 107, 117–127.

Bywater, R. P., Conde-Frieboes, K. Did life beginon the beach? Astrobiology 2005, 5, 568–574.

Chang, I.-F., Szick-Miranda, K., Pan, S., Bailey-Serres, J. Proteomic characterization of evo-lutionary conserved and variable proteins ofArabidopsis cytosolic ribosomes, PlantPhysiol. 2005, 137, 848–862.

Chen, I. A., Roberts, R.W., Szostak J.W. Theemergence of competition between modelprotocells, Science 2004, 305, 1474–1476.

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Delaye, D. Becerra, A., Lazcano, A. The lastcommon ancestor: what’s in the name, Orig.Life Evol. Biosph. 2005 35, 537–554.

DeDuve, C. A research proposal on the originof life, Orig. Life Evol. Biosph. 2002, 33,559–574.

Deamer, D., Dworkin, J. P., Sandford, S.A.,Bernstein, M. P., Allamandola, L. J. Thefirst cell membranes, Astrobiology 2002, 2,371–381.

Doolittle, W. F. Phylogenetic classification andthe universal tree, Science 1999, 284, 2124–2128.

Eigen, M. The origin of genetic information:viruses as models, Gene, 1993, 135, 37–47.

Ferris, J. P. Montmorillonite catalysis of 30–50mer oligonucleotides: laboratory demon-stration of potential steps in the origin of theRNA world, Orig. Life Evol. Biosph. 2002, 32,311–332.

Forterre, P. The two ages of the RNAworld, andtransition to theDNAworld: a story of virusesand cells, Biochim. 2005, 87, 793–803.

Forterre, P., Confalonieri, F., Charbonnier, F.,Duguet, M. Speculation on the origin of lifeand thermophily: Review of available infor-mation on reverse gyrase suggests that hy-perthermophilic procaryotes are not soprimitive, Orig. Life Evol. Biosph. 1995, 25,235–249.

Gil, R., Silva, F. J., Pereto, J., Moya, A. Deter-mination of the core of the minimal bacte-rial gene set. Microbiol. andmolec, Biol. Rev.2004, 68, 518–537.

Hanczyc, M.M., Szostak, J.W. Replication ofvesicles as models of primitive cell growthand division. Current Opin., Chem. Biol.2004, 8, 660–664.

Jeffares, D. C., Poole, A.M., Penny, D. Relictsfrom the RNA world, J. Mol. Evol. 1998, 46,18–36.

Joyce, G. F. The antiquity of RNA-based evo-lution, Nature 2002, 418, 214–221.

Kanavarioti, A., Monnard, P.-A., Deamer,D.W. Eutechtic phsces in ice facilitate non-enzymatic nucleic acid synthesis, Astrobiol-ogy 2001, 1, 271–281.

Kapp, L. D., Lorsch, J. R. The molecular me-chanics of eukaryotic translation, Ann. Rev.Biochem. 2004, 73, 657–704.

Koonin, E., Martin, W. On the origin of ge-nomes and cells within inorganic compart-ments, Trends Genet. 2005, 21, 647–654.

Lathe, R. Tidal chain reaction and the origin ofreplicating polymers, Int. J. Astrobiol. 2005,4, 19–31.

Lehto, K., Karetnikov, A. Relicts and modelsof the RNA world, Int. J. Astrobiol. 2005, 4,33–41.

Liang, H., Landweber, L. F. Molecular mimi-cry: quantitative methods to study structuralsimilarity between protein and RNA, RNA2005, 11, 1167–1172.

Maizels, N., Weiner, A.M. Phylogeny fromfunction: evidence from the molecular fossilrecord that tRNA originated in replication,not translation, Proc. Natl. Acad. Sci. USA1994, 91, 6729–6734.

Martin, W., Russell, M. J. On the origin of cells:a hypothesis for the evolutionary transfor-mation from abiotic geochemistry to che-moautotrophic prokaryotes, and from pro-karyotes to nucleated cells, Phil. Trans. R.Soc. Lond. B. 2002, 358, 59–85 (also in:www.gla.ac.uk/project/originoflife/html/2001/pdf_files/Martin_&_Russell.pdf).

Mojzsis, S. J., Arrhenius, G., Keegan, K. D.,Harrison, T.M., Nutman, A. P., Friend,C. R. L. Evidence for life on Earth before3,800 million years ago, Nature 1996, 384,55–59.

Orgel, L. E. Prebiotic chemistry and the originof the RNA world, Crit. Rev. Biochem. Mo.2004, 39, 99–123.

Pennisi, E. Is it time to uproot the tree of life,Science 1999, 284, 1305–1307.

Poole, A., Penny, D., Sjçberg, B-M. Methyl-RNA: an evolutionary bridge between RNAand DNA? Chem. Biol. 2000, 7, R207–R216.

Poole, A., Jeffares, D., Penny, D. Early evolu-tion: prokaryotes, the new kids on the block,BioEssays 1999, 21, 880–889.

Poole, A.M., Jeffares, D., Penny, D. The pathfrom the RNA world, J. Mol. Evol. 1998, 46,1–17.

Sanders, P. G.H. Chirality in the RNA worldand beyond, Int. J. Astrobiol. 2005, 4, 49–61.

Schmidt, G., Christensen, L., Nielsen, P. E.,Orgel, L. E. Information transfer from DNAto peptide nucleic acids by template-directedsyntheses, Nucleic Acids Res. 1997, 25, 4793–4796.

Steitz, T. A., Moore, P. B. RNA, the firstmacromolecular catalyst: the ribosome is aribozyme, Trends Biochem. Sci. 2003, 28,411–418.

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Tian, F., Toon, O. B., Pavlov, A. A., De Streck,H. The hydrogen-rich early atmosphere,Science 2005, 308, 1014–1017.

Vlassov, A. V., Johnston, B. H., Landweber,L. F., Kazakov, S.A. Ligating activity offragmented ribozymes in frozen solution:implications for the RNA world, Nucl. AcidsRes. 2004, 32, 2966–2974.

W�chtersh�user, G. From pre-cells to Eukarya– a tale of two lipids,Mol. Microbiol. 2003, 47,13–22.

Watson, E. B., Harrison, T.M. Zircon ther-mometer reveals minimum melting condi-tions on earliest Earth, Science 2005, 308,841–844.

Weiner, A.M., Maizels, N. The genomic taghypothesis: modern viruses as molecular

fossils of ancient strategies for genomicreplication, and clues regarding the originof protein synthesis, Biol. Bull. 1999, 196,327–330.

Westall, F. Life on the early Earth: A sedi-mentary view, Science 2005, 308, 366–367.

Woese, C. R. The universal ancestor, Proc. Natl.Acad. Sci. USA 1998, 95, 6854–6859.

Woese, C. R., Kandler, O., Wheelis, M. L. To-wards a natural system of organisms: Pro-posal for the domains Archaea, Bacteria andEucarya, Proc. Natl. Acad. Science USA 1990,87, 4576

Yang, S., Doolittle, R. F., Bourne, P. E. Phy-logeny determined by protein domain con-tent, Proc. Natl. Acad.Sci. USA 2005, 102,373–378.

4.9Questions for Students

Question 4.1What are the difficulties in understanding of the origin of life?Question 4.2

What are the building blocks of life and how do they assemble to make functionalcells?Question 4.3

What are the putative steps required for the establishment of self-sustainable life?Question 4.4Explain the RNA world.Question 4.5What kind of conditions might have driven the prebiotic molecular evolution

towards life?Question 4.6What can we say of the LUCA and of the differentiation of the three domains of

life from LUCA?Question 4.7How do you define the beginning of life?

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6HabitabilityCharles S. Cockell

The term “habitability” means many different things depending onthe organisms that are considered, as it defines the chemical andphysical envelope for a given organism. Because there is currentlyno direct evidence for life on another planet, habitability is neces-sarily constrained by our knowledge of life on Earth. We use ourknowledge of the extremes of life on Earth to assess extraterrestrialenvironments and the plausibility that they can support life. In thischapter the use and limitations of the concept of habitability arediscussed and examples are provided of how the habitability ofother worlds is assessed using extreme environments on Earth.The chapter starts with a brief discussion of the history of habit-ability, including some historical watersheds in this concept. Then,some of the factors and mechanisms that determine the habit-ability of other planets are discussed. Finally, a postulate for hab-itability is given, which can be used to guide the way we think aboutthe characteristics of other environments that we wish to assess ashabitable or uninhabitable.

6.1A Brief History of the Assessment of Habitability

The assessment of the “habitability” of other planetary bodies has been a pervasiveintellectual problem throughout the history of planetary sciences and biology.Indeed, erroneous assertions of habitability, borne of optimism about the prospectsfor life, have clouded attempts to make astrobiology a serious field of scientificendeavor. In any field of science where technical or logistical constraints limit theamount of data that can be acquired, it is necessary to proceed with caution.Ultimately, the way in which we define habitability, the factors that determine it,and the way we use instrumentation to assess the habitability of other planetsunderpin the entire astrobiological enterprise. As efforts are developed to search

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for “Earthlike” planets around distant stars (extrasolar planets), understandingwhat constitutes habitability has become an area of great relevance.Prior to the invention of the telescope, the only planetary body that provided any

detailed information on its surface characteristics was the Moon. Mars was a redanomaly in the night sky, but this color, spread across a tiny disk, did not revealdetails. The pre-telescope era and the view of habitability it engendered was an erathat I call the Birth of Optimism. This period of optimism was one dominated bytheoretical discussions on the plurality of worlds. The debate was infused byreligious considerations (i.e., that humans were special and unique) and contrast-ing considerations more at home in natural sciences (i.e., the notion of “plen-itude”) that nature makes use of all possibilities and, therefore, other worlds wouldbe inhabited like ours.The Birth of Optimism is marked by some remarkable comments and assertions

that would not be considered out of place in today’s debates on habitability. Amongthe most notable is the comment by the Greek philosopher Metrodorus of Chios, astudent of Epicurus, who in the fourth century B. C. stated: “It would be strange if asingle ear of corn grew in a large plain, or there were only one world in the infinite”(citation in Cornford 1934). The Roman poet Lucretius similarly stated: “It is in thehighest degree unlikely that this Earth and sky is the only one to have beencreated.”These general, but important, thoughts were also surrounded by an entourage of

more-specific claims and beliefs concerning the inhabitants of the Moon. ManyGreeks and Romans believed that the Moon was inhabited by intelligent beings.One would have thought that the invention of the telescope in the 17th century

would have provided a means to assess the habitability of other planets moreaccurately, thus leading to a reduction in speculation as worlds yielded their secretsto empirical observation. However, the opposite occurred. Early telescopes allowedthe discs of new worlds to be resolved, but their power was not sufficient to be ableto tell anything about their surfaces or their environmental conditions. The 17th

and 18th centuries were thus a time when optimism ran riot. This was a periodwhen we knew of the existence of countless worlds, from Mars to the Jovian andSaturnian moons, but we knew little about the physical conditions in the SolarSystem. I call this period, which runs right up to the 1960 s, the Age of Optimism.It is misleading to summarize such a long period of history with just a few

quotes, but to give some flavor of the time and the way in which the telescope madepossible observations of other planetary bodies without an ability to assess theirhabitability, a few quotes are worthwhile, which are taken from an extensive reviewby Crowe (1999). French author Bernard le Bovier de Fontenelle (1657–1757) statedof the Venusians that they were “little black people, scorched with the Sun, witty,full of fire.” British astronomer William Herschel (1738–1822), whose observatio-nal astronomy was par excellence, informs us: “By reflecting a little on this subjectI am almost convinced that those numberless small Circuses we see on the moonare the works of the Lunarians and may be called their Towns.” And as recently as1909, in his book Mars as the Abode of Life, Percival Lowell asserted: “Everyopposition has added to the assurance that the canals are artificial; both by

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disclosing their peculiarities better and better and by removing generic doubts as tothe planet’s habitability.”The Age of Optimism is a fascinating age for the discussion of the habitability of

other worlds, but it is also a warning from the past. Enveloped in an era wheremany scientists had optimism about the habitability of other planets, none of thecomments listed above seemed absurd to their authors, despite their lack ofempirical data to support their claims. To them it was just obvious that otherplanets were inhabited. It was a case of culture driving science. Today, we aresimilarly living through a period of optimism that, although more constrained byempirical observations from spacecraft and telescopes, is nevertheless stronglydriven by an undercurrent of new-found optimism in the likelihood of life else-where.The 1960 s witnessed the beginning of the space age and, with it, the possibility

of visiting other planets with spacecraft. I call this age of the discussion ofhabitability, which runs until the early 1990 s, the Age of Retreat. The failure tofind canals on Mars, culturally sophisticated Venusians, or fortresses on the Moon,irrefutably supported by landers and orbiters, forced a retreat in our view ofhabitability. We realized that many of these worlds we had viewed through rose-tinted biological spectacles were in fact cold or hot, barren wastelands with little orno prospects for any life at all. The Viking landers did nothing to dispel the vision ofMars as a barren, dead planet (see Chapter 5). Despite the somewhat negative viewof habitability, this period of space exploration was nevertheless remarkable,leading to new and astonishingly detailed insights into the conditions on otherplanetary surfaces. Images sent back from the far reaches of the Solar System bythe Voyager robots, for instance, truly ushered in an extraordinary period ofexploration. Of course, habitability, at least in the case of the moon, was alsodirectly assessed by human explorers during this period.Despite the biologically disappointing data sent back from other planets, there

was still room for maneuvering. The period from the 1990 s onwards I refer to asthe Rebirth of Optimism. Two developments came together to generate renewedoptimism in the possibility of life in our Solar System. Firstly, spacecraft instru-ments became of better quality and had higher resolution. Where previously wesaw barren Martian deserts with some evidence of past liquid water, we now sawextant ice sheets and even putative gullies formed by liquid water (see Chapter 8).Rocky moons around Jupiter yielded images of ice sheets, and studies of themagnetic fields around them suggested liquid water oceans that are conducive tolife (see Chapter 10). The array and sophistication of instruments on spacecrafthave provided many different imaging methods, which together have providedinsights into environments on other planets that may be conducive to life.Secondly, studies of microorganisms on Earth expanded the envelope of life to

such an extent that many environments on Earth, previously thought to be unin-habitable, were found to harbor life (see Chapter 5). Some of these environmentsoverlap with extraterrestrial planetary environments in some physical and chem-ical conditions. Because they contain life on Earth, renewed optimism about theircapacity to sustain life elsewhere has been encouraged. Such environments include

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permafrost in Earth’s polar regions, which may be analogous to permafrost regionson Mars, and hydrothermal vents on the ocean floors and ocean-spreading axes,which have been suggested to provide insights into the biological potential of thebottom of Europa’s oceans (see Chapter 10).In Fig. 6.1 I have drawn a graph showing, qualitatively, the change in optimism

about habitability over time. The current challenge in astrobiology is, of course, todetermine the direction in which we should extrapolate this graph and whether wecan transgress from “optimism” to the positive identification of life on particularplanetary bodies.This brief review of the history of habitability is lacking in many details, as there

is insufficient space to review adequately the many diverse discussions since thetime of the ancient Greeks. However, it should provide some understanding of themajor periods of history in the assessment of habitability, from which moredetailed research can be undertaken. It should also place in context where thestudent of astrobiology stands today in this long history, and how we have arrived atwhere we are.

6.2What Determines Habitability?

The habitability of an environment is firstly, and quite obviously, constrained bythe organisms we wish to contemplate in the environment under consideration.The two end members of habitability considerations are extremophilic micro-organisms, which define the outer boundaries of life, and humans and othercomplex multicellular organisms, which require much more narrow ranges ofenvironmental conditions. In between them is a diversity of prokaryotes andmulticellular organisms that may be adapted to specific extreme environmentsand have different environmental tolerances. Table 6.1 shows some environmentaltolerances of humans and microbes to illustrate this difference in ranges (see alsoChapter 5).

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Fig. 6.1 Qualitative graphshowing the change in ourviews of habitability over time.

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Table 6.1 Some physical and chemical factors important fordefining whether an environment is habitable and the rangestolerated by microorganisms and humans.

Parameter Microorganisms Humans[a]

Temperature < 0–121�C 0–30�CPressure <50 hPa–>10 000 hPa[b] 700 hPa–5 000 hPaRadiation 4 000 Gy[c] 1–3 Gy[c]

pH 0–13 Near neutralOxygen 0–~100% 15–25%Carbon dioxide 0–100% <1%

Source: Some of these values are taken from McKay et al. 1991.a Some of these values are approximations. For example, humans can tolerate a far wider

temperature range than shown here by using technology, and a wide range of pHs can betolerated by humans over short time periods.

b 1 hPa = 1 mbarc Sublethal dose; 1 Gy (Gray) = 100 rad

Given the obvious need to define the types of organisms we are considering, whatare the fundamental requirements for any life forms based on what we know aboutlife on Earth? All life must have a solvent to carry out chemical reactions (and to actas a reactant itself). At least based on life on Earth, this solvent is water, and thusany planetary environment we postulate to be habitable must have liquid water (seeChapter 1). The presence of liquid water on a planetary surface has often beentaken, alone, to be the definition of “habitable.” The “habitable zone” around a staris defined as the region around a star where liquid water is stable on a planetarysurface (see Section 6.4.1). It should be noted that this classic definition of ahabitable zone is based on liquid water made possible as a result of direct solarheating from the parent star. In comparison, the Jovian moon Europa lies faroutside the classic habitable zone but has a liquid water ocean on account of thetidal heating of the moon.There must be an energy supply to drive the reactions that life requires to grow,

reproduce, and repair itself. Energy supplies can range from chemolithotrophicmetabolism (using inorganic redox couples such as reduced iron and nitrate todrive energy acquisition) to heterotrophic modes of metabolism (using organicmolecules to provide energy) to photosynthesis (using photons from the parent starto drive energy acquisition) (see Chapter 5).There must be a source of nutrients in an accessible form, with which life can

construct itself. On Earth, we know these to be carbon, hydrogen, oxygen, nitrogen,sulfur, and phosphorus (C, H, O, N, S, P). Many organisms use more than thiscomplement of elements. Elements as diverse as iron, zinc, and molybdenum canbe required, and many anaerobic microorganisms on Earth are known to requiretungsten and selenium in their culture medium. However, whether many of theseare absolutely required for life (as opposed to being an evolutionary quirk ofenzymes and other biochemical systems on Earth) is not understood. At least as

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a minimum we suppose that life requires those six elements as summarized inCHONSP.A planetary environment that possesses all three of these requirements, i.e.,

water, energy, and basic nutrients, can be presumed to be a place that is potentiallyhabitable. Although one can postulate entirely novel biochemistries that might usecompletely different elements and solvents (such as silicon-based life or life usingammonia as a solvent), because no such life has yet been found, it does not fitwithin the boundaries of science. It goes without saying that the discovery of anovel biochemistry using other types of elements and solvents on another planetcould simply be used to expand the definition of habitability. At the present timewe use life on Earth to define its boundaries. In Section 6.4 two of these factors thatdetermine the boundaries, i.e., temperature and energy, are considered.

6.3Uninhabited Habitable Worlds

It is important to understand that the presence of habitable conditions does notimply that an environment is inhabited. On Earth, where the conditions describedabove are met, microorganisms are invariably found, because there is a plenitudeof microorganisms inhabiting many diverse environments. For example,4–6 � 1030 microorganisms are estimated to exist on Earth. The appearance of ahabitable environment offering conditions for life usually leads to its rapid colo-nization. However, on young planets or planets where, for whatever reasons, lifehas not originated, one could imagine habitable environments where life would notbe around to take advantage of the conditions, particularly if these environmentswere transient, such as a warm hydrothermal system in an impact crater on anotherwise frozen, dead world. Such environments are “uninhabited habitablehabitats,” and determining their distribution throughout the Universe is a chal-lenge of astrobiology.

6.4Factors Determining Habitability

6.4.1Habitability and Temperature

The temperature of the surface of a planetary body is, in principle, simply deter-mined by the heat it receives from its star in the form of visible and near-infrared(IR) light and the energy it releases in the form of thermal IR radiation. Thesolution of these simple inputs and outputs yields a “black body” temperature for aplanetary surface. Although this simple formulation works quite well for a plan-etary body without an atmosphere, an atmosphere can cause a warming effect bytrapping IR radiation, the so-called greenhouse effect. In the case of the Earth,

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water and carbon dioxide provide the greatest contribution to warming. Morerecently, anthropogenic greenhouse gases, such as chlorofluorohydrocarbons(CFCs), have contributed to the global warming. The greenhouse effect is itselfgreatly complicated by the quantity of dust in an atmosphere, the cloudiness, andthe possible presence of chemical smog, all of which will influence the magnitudeof the effect. In the case of the Earth, the greenhouse effect is sufficiently large tobring our planetary surface temperature to above freezing (about 15 �C average),whereas otherwise it would be below freezing, demonstrating quite effectively therole of greenhouse gases in influencing surface habitability.The temperature of a planetary surface will be influenced by many feedback

processes, both positive and negative. Snow cover, for instance, will increase thealbedo (reflectivity) of a planetary surface, thus causing greater emissions of IRradiation back into space, cooling the planet further.This positive feedback is suggested to be responsible for the onset of “snowball

Earth” conditions, whereby runaway growth of ice sheets, which increase thealbedo and drive further cooling, ultimately cause a freeze-over of all, or most, ofthe planetary surface. These snowball Earth episodes are postulated to haveoccurred during the Proterozoic (2.5–0.54 billion years ago). One of these events,which occurred in the period between 2.45 and 2.2 billion years ago, is thought tobe linked to the rise in atmospheric oxygen at that time; the oxygen may havereacted with methane (another greenhouse gas) in the atmosphere, reducing thegreenhouse effect and leading to glaciations. There is evidence for snowballglaciations in the late Proterozoic as well. The existence of widespread evidencefor glaciers during these periods is also supported by modeling studies. Theseglaciations provide dramatic empirical evidence for the importance of the ice andsnow albedo feedback.Another feedback effect is controlled by water vapor. Because water vapor

contributes to greenhouse warming, it too can cause positive feedback. As theplanet warms, more water evaporates from the oceans into the atmosphere andcauses yet more warming. Conversely, cooling of the surface reduces evaporationand reduces the greenhouse effect caused by water vapor.The extent to which these feedback processes would be important on other

planets obviously depends on their mean temperature, which will influence theextent of ice and snow on their surfaces. It also depends on their inventory of waterand thus the size of their oceans and the extent to which water evaporation drovethe greenhouse effect. Therefore, we can see that although the principles are quiteeasy to grasp, applying habitability criteria to other planets would require a specificknowledge of each body being assessed.The ice/snow and water vapor feedback processes function over quite short

timescales (almost instantly), but there are other feedback processes that operateover millions of years and are profoundly important for determining the habit-ability of a planet. One of the most important of these is the carbonate–silicatecycle.The carbonate–silicate cycle regulates the amount of CO2 in the atmosphere and

thus the contribution of this gas to the greenhouse effect. The CO2 in the

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atmosphere is there mainly as a gas, but some of it is dissolved in atmosphericwater as carbonic acid (H2CO3). When it rains, this weak acid washes over silicaterocks and dissolves them. The product of the weathering process is bicarbonate(HCO3

–), which itself is washed into the oceans. Bicarbonate is used by diverseorganisms for photosynthesis and to make calcium carbonate shells, e.g., those ofthe foraminifera. This CO2 is thus locked up in these carbonates and effectivelyburied and removed from the atmosphere. The continuous operation of thisprocess would, of course, remove all the CO2 from the atmosphere and cool theplanet, but the CO2 fixed as carbonates is eventually returned to the atmosphere.Deep in the crust, plate tectonics pushes the carbonates into high-pressure andhigh-temperature regions where it reacts with silicate rocks, releasing the CO2 backinto the atmosphere through volcanism, and hence the cycle is complete.With this in mind, we can now understand how the carbonate–silicate cycle

works to regulate the surface temperature of a planet. If the planet slowly heats up(e.g., by the slowly increasing solar luminosity over time), the weathering rate isincreased at the planetary surface (because chemical reactions occur faster athigher temperatures), and thus more CO2 is drawn down from the atmospherein these reactions. The greenhouse effect is thus reduced and the temperaturedrops. Conversely, cooling reduces the weathering rate and less CO2 is drawndown. Because volcanism is still returning the existing CO2 pool back into theatmosphere at the same rate, the atmospheric CO2 concentration rises and thegreenhouse effect is increased, thus warming the planet. Thus, we can see how thecarbonate–silicate cycle provides a negative-feedback control of planetary temper-ature.The importance of the carbonate–silicate cycle for habitability can be easily

appreciated by observing Mars and Venus (see also Chapter 8). Mars long agoceased to have plate tectonics. The presence of remnant magnetic regions on Marssuggests that it may have had some plate tectonics, but the small size of the planetcaused it to rapidly cool. The shutdown of widespread volcanism would haveprevented CO2 from being rereleased into the atmosphere, thus rendering thecarbonate–silicate cycle inactive. Combined with this problem is the problem ofkeeping Mars warm at the further distance it occupies from the Sun, which makesthe CO2 greenhouse less effective to the point where sufficient CO2 to keep theplanet warm would cause it to condense out (although other solutions such as ahydrocarbon smog and CO2 ice clouds might solve this problem). Thus, even if anyputative carbonates could be returned by volcanism, the greenhouse effect hasserious problems in operating on Mars. The result is a planet that today has a meantemperature of –60 �C, although the subsurface may have environments conduciveto life.By contrast, Venus has a very different problem. Volcanism is still evident on the

planet; therefore, unlike on Mars, the return of CO2 to the atmosphere does notseem to be a problem. However, the high temperature of Venus long ago causedthe complete evaporation of its water inventory. The water was eventually lost intospace from the top of the atmosphere, thus shutting down weathering. With noway for the CO2 to react in surface weathering reactions with silicate rocks

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mediated by water, all of the CO2 remained in the atmosphere, leading to the 464 �Cmean temperature now found at its surface. The atmospheric CO2 content woulditself have contributed to greenhouse warming, thus accelerating the loss of water.Although there is necessarily some simplification in these accounts, we can see

how the carbonate–silicate cycle can be used to understand some quite fundamen-tal reasons for the conditions of habitability on Venus andMars. Venus provides uswith an inner bound at which the carbonate–silicate cycle becomes ineffective anda planet is transformed into a scorched desert. Mars can be seen as a proxy for theouter bound of habitability. These bounds can therefore be conveniently used todefine the region around a star where the liquid water is stable on a planetarysurface within temperature conditions conducive to life.Some of the simplifications in this account include the role of plate tectonics. For

example, if Mars were larger than it is, it is possible that it would retain afunctioning carbonate–silicate cycle on account of the presence of plate tectonics,leading to a cycle of carbon and a less extreme loss of its atmosphere in its earlyhistory. Might a larger Mars have resulted in a second habitable world in our ownSolar System? Thus, the bounds of habitability within a star systemmust be treatedas somewhat of an approximation.In addition, we should bear in mind that mechanisms other than the carbonate–

silicate cycle might influence the stability of liquid water. The tidal forces exerted byJupiter on its moon Europa, for example, allow for the stability of liquid waterunder a thick ice sheet, independent of the carbonate–silicate cycle’s temperatureregulation (see Chapter 10). Europa lies well outside the traditional habitable zonedefined by solar luminosity. Nevertheless, the habitable zone provides a convenientmethod to help define regions around other stars that might support liquid water,and it helps us to understand how conditions on a planetary surface, down to thescale of microorganisms, can be defined by feedback processes operating over longtime periods.Figure 6.2 shows a diagram of where the habitable zone lies around different

stars. This zone is much the same size when the distance from the star is plotted onthe logarithmic scale.Stars cooler than our own Sun, such as M stars, have habitable zones that are

closer to their star, because planets need to be closer in for the greenhouse effect towork sufficiently. Hotter stars, such as F stars, have habitable zones that are furtheraway. For very cool stars, a complication arises in that if the planet is too close to thestar it becomes tidally locked, meaning that only one side is facing towards the star.Although this might cause the dark side of the planet to freeze out, causing theatmosphere to collapse, if the atmospheric transport of heat is sufficient, this maynot occur. It raises the intriguing possibility of life on planets where photosynthesisis possible only on one side and life forms on the other side live in perpetualdarkness.In our own Solar System the inner region of the habitable zone is thought to lie

at about 0.95 AU and the outer region somewhere between 2.37 and 2.4 AU(AU = astronomical unit = average distance of the center of the Earth from thecenter of the Sun = approximately 149.6 � 106 km) (Fig. 6.2).

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A further augmentation of the habitable zone is the “continuously habitablezone” (CHZ). This is the region around a star where conditions for habitability aremet over some defined period of time. For example, because we know that it hastaken 3.5 billion years to go from microorganisms to intelligent life on Earth (seeChapter 1), a search for planets around other stars might focus on regions wherethe habitable zone exists for at least this length of time. This is especially necessaryif one wants to search for radio signals from other civilizations, e.g., the projectSearch for Extraterrestrial Intelligence. Shorter lengths of time for the existence ofthe CHZ might be sufficient for the rise of oxygen and thus the possible detectionof oxygen in the atmosphere of extrasolar planets.

6.4.2Habitability and Energy

For a planetary surface to be habitable, itmust also have a supply of energy. At least formuch of life on Earth, this energy is derived from the flow of electrons through abiologically mediated electron transport chain. The fundamental chemical processthat drives energy acquisition is called the “chemiosmotic theory.” Electron transportthat occurs during redox reactions expels protons from the cell membrane. Thistranslocation process creates a proton gradient across the cellmembrane. The protonscan move back across the cell membrane to do useful work, e.g., adenosine triphos-phate (ATP) synthesis (seeChapter 4). Thus, tomake energy for growth, reproduction,and repair, most life must have access to electron donors, which supply electrons andelectron acceptors, which take up electrons in order to drive the energy-yieldingreactions. Examples of these electron transfer reactions are shown in Fig. 6.3.

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Fig. 6.2 Habitable zone (boxed area) around other stars as afunction of the mass of the star and the distance from the star.M� = Solar mass; the long dashed lines delineate the probableterrestrial planet accretion zone (figure is taken from Kasting etal. 1993).

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Inorganic redox couples perhaps represent the most widespread form of energyavailability. Many of these elements or compounds are formed in supernovae andexist in stars. Figure 6.4 shows oxygen and iron in the Sun, which can be used byiron-oxidizing microorganisms as a source of energy (they require reduced iron).The Sun is obviously not habitable because it has no water and is too hot, but thisgraph nicely illustrates the universally widespread distribution of energy sourcesfor life.Many microorganisms can use reduced iron as an electron donor and com-

pounds such as nitrate and oxygen as electron acceptors. Because electron donorsand acceptors are inclined to react through abiotic processes (e.g., reduced iron“rusts” in the presence of oxygen), having a supply of electron donors and acceptorsrequires some type of geochemical disequilibrium where both electron donors andacceptors can be continuously produced, coexist, and be available for life. Activevolcanism, plate tectonics, and asteroid and comet impacts are examples of proc-esses that can cause turnover and movement in the planetary surface and subsur-face, generating geochemical gradients that life can take advantage of.Furthermore, some inorganic redox reactions occur very slowly because of a high

activation energy; in this case, life can overcome these activation energies andincrease the rate of the energy-yielding reaction.The range of energy-yielding processes on Earth is immense. As well as those

reactions shown in Fig. 6.3, which are used by chemolithoautotrophs (literally“rock eaters”), other organisms rely on heterotrophy (using organic carbon as asource of energy – including direct ingestion of prey and fermentation) and stillothers, i.e., photoautotrophs, use sunlight as a source of energy and derive elec-trons from water.

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Fig. 6.3 Examples of energetically favorable reactions forthe acquisition of energy by microorganisms. The downward-pointing arrows indicate thermodynamically favorable reactions.

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In the case of fermentation, the production of energy relies on the breakdown oforganic molecules without an electron acceptor being involved – the molecules areessentially dismutated with a release of energy and no overall change in the redoxlevels of the substrate and products. In that sense, fermentation differs from othertypes of energy-yielding processes.The photoautotrophs produce sugars from the reaction of carbon dioxide and

water according to the classic reaction in Eq. (6.1). Here, light energy is used toactivate chlorophyll or bacteriochlorophyll, which then provides an electron to theelectron transport chain.

6 CO2 + 6 H2O + light energy� C6H12O6 + 6 O2 (6.1)

The sugars produced in this reaction are then available for other organisms torespire (burn) in oxygen again, thus yielding the energy locked up in the sugars.To a large extent, the biosphere we know of on Earth is made possible by

photoautotrophs. Without them the biosphere would probably have a productivity

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Fig. 6.4 Relative abundance of chemical elements in theatmosphere of our Sun. The graph indicates that redox couplesfor energy production are widespread throughout the Universe.

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much less than about 2% of its current productivity, and the planet would berelegated to chemolithoautotrophs living off rocks and heterotrophs living off theorganics they produce. The existence of “complex” multicellular life is dependenton photosynthesis, because photoautotrophs provide the biologically bound carbonand oxygen that make possible the sorts of energy-yielding reactions required forlarge organisms to operate. The rise in atmospheric oxygen, which seems to haveoccurred about 2.4 billion years ago (Fig. 6.5), was the result of photosynthesis,

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Fig. 6.5 Bounds of oxygen concentrations during the history ofthe Earth. The innovation of using sunlight as a source of energyand water as an electron donor resulted in the formation ofoxygen. Eventually, levels of the gas were sufficient to change theatmospheric composition of the planet (1 bar = 1000 hPa;Ga = billion years) (from Catling with permission)

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allowing for the widespread use of this oxidant. Thus, it is important to rememberthat habitability can also be influenced, even determined, by organisms them-selves.Each successive group of organisms inhabiting the Earth may change the

conditions in such a way that it influences the environmental conditions andthereby the nature of the organisms that follow them. In that sense, habitabilityis not merely a function of planetary chemical and physical conditions but is alsopredicated on the course of biological evolution that preceded any given point inthe planet’s history. This course of evolution, at least on Earth, has been stronglycoupled to life’s mechanisms for gaining energy, photosynthesis having had themost profound effect on planetary habitability.The minimum energy that life can use on Earth is set by the energy needed to

make ATP, which is essentially the energy currency molecule used by life. ATP is achemical form of energy. The minimum energy that life on Earth seems capable ofexploiting is 20 kJ mol–1, although studies on hydrogen production and consump-tion in sediments suggest that much lower energy availabilities might be exploitedby life. The degree to which energy-yielding reactions used by life on Earthrepresent the “universal” set of energy-yielding possibilities is not known. Never-theless, life on Earth has mastered a vast array of reactions, and almost everyavailable redox reaction known, at least amongst chemolithoautotrophs, has beenshown to have a corresponding organism that uses it. Any planet that has sourcesof energy in the form of organic molecules, inorganic redox couples, or plentifulavailability of light and carbon dioxide can be presumed to be habitable with respectto energy availability.

6.4.3Other Factors that Determine Habitability

Still other factors may be important for determining habitability and its character-istics over the lifetime of a planet. Many of these other factors are contentious andopen to contrary interpretations. For example, the Moon is thought to stabilize theEarth’s obliquity. Thus, without it the Earth’s obliquity would swing wildly overtens millions of years from 0� to 85 �. One might argue that this would make theEarth less habitable by causing dramatic climate changes. One could equally arguethat by causing frequent climate change, the lack of a moon would be a selectionpressure for generalist organisms that were not so sensitive to rarer climatechanges and were more likely to have longer species lifetimes because of theirability to withstand a greater range of environmental changes. Perhaps extinctionswould be less common.Other factors that influence habitability include the impact flux and the magni-

tude of objects that hit a planet of a given size, which will determine the extent towhich surface habitats and the atmosphere are perturbed. Further, the ratio ofoceans to land might influence the availability of oceanic and land-based environ-ments for the origin and evolution of life.

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Determining which factors are essential for habitability and which are not issubject to anthropocentric interpretations colored by our own evolutionary path.Thus, care must be taken. However, the assertion that the availability of a solvent,energy, and nutrients is the minimum requirement for an environment to behabitable seems to be a safe proposition.

6.5A Postulate for Habitability

As the brief review of the history of our perception of habitability has shown, apervasive problem in biology is assessing the habitability of planets for which thereis a limited dataset. The expense and logistical difficulty of launching missions toother planets and moons necessitates drawing biological conclusions based onvastly fewer data than are available for habitats on Earth.On Earth, at least, we can approach the question of whether habitats are

habitable or uninhabitable by two means. Firstly, we can directly explore the regionin question. Because most regions of the Earth are accessible multiple times withinthe budgets that can be acquired through research grants, it is possible forscientists to assess the habitability of environments directly. Initial datasets canbe reviewed by returning to the site of interest. Secondly, environments can beassessed by using as analogies environments that have been explored previouslyand that are known to possess very similar physical and chemical characteristics.Thus, a comparison of certain unexplored habitats to similar explored habitats onEarth allows an extrapolation of habitability criteria (surfaces for growth, liquidwater, nutrients, light, etc.) to other habitats.The assessment of actual or past habitats on other planets poses quite different

problems for a number of reasons:• It is, for the time being, logistically difficult for scientists to

directly visit extraterrestrial sites of interest themselves.• The data that do exist are limited and may have been acquired

by just a few spacecraft measurements or by observationsfrom Earth, thus greatly limiting the empirical basis of as-sessment of habitability.

• The data gathered do not necessarily have a biological focus,because that might not have been the focus of the missions inthe first place. For example, the concentration of the majormacronutrient nitrogen (in its various biologically accessiblestates) in the Martian regolith is unknown, despite the nu-merous landers that have been to Mars and the obvious bio-logical importance of this measurement.

• Extraterrestrial environmental conditions are often very dif-ferent from conditions known to support life on the presentEarth, frustrating any analogue parallels that can be used toassess the possibility for life. An obvious example is surface

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atmospheric pressure and composition, which is different forMars, Venus, and Earth (see Chapter 8).

We can use the present-day Earth as our point of reference. However, the Earthitself evolved through time and so did its habitability. In this respect, the early Earthcan be regarded as a different planet, and the problems associated with theassessment of its habitability are similar to those that challenge us regarding theother terrestrial planets. These problems are related to the fact that although wehave unlimited access to the locations where the oldest well-preserved rocks occur(about 3.5 billion years for evidence of life), the dataset is limited because

• there are only two localities where these ancient rocks areexposed (the greenstone belts of Barberton in South Africaand the Pilbara in Australia);

• these ancient terrains are already relatively young, havingformed a billion years after the formation of the Earth; and

• the evidence for potential life in these rocks is disputed and,consequently, so is the habitability of the Earth at that time(see Chapter 1).

The scarcity of the data points is related to the dynamics of a tectonically activeplanet where the process of lateral plate tectonics has caused the destruction of theoldest rocks.In view of the inherent complexities in making comparisons between present-

day Earth and other planets, including early Earth, one useful approach to theproblem is to define a postulate that can be used to guide attempts to makecomparisons and to arrive at conclusions on habitability and the likelihood of life.Owing to the different environmental conditions occurring on other planets

compared to the Earth, and to the limited number of datasets available fromspacecraft and Earth observations, it is necessary to create a bridge between whatwe know about habitats on Earth at present and the environment under consid-eration (Fig. 6.6).In the case of early Earth the “astrobiological gap” in the assessment of habit-

ability can be filled by visiting the remnants of early Earth or in the case ofextraterrestrial environments, by visiting the planet under study. Thus, the ques-tions that remain about the habitat being studied can be directly addressed.However, if the database is poor, as in the situation of the early Earth, or if it is

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Fig. 6.6 Astrobiological gap in knowledge between present-dayEarth habitats and extraterrestrial or early Earth habitats.

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not logistically easy to visit the planet in question, the gap must be filled by usingthe existing data.Historically, in the literature the gap between extraterrestrial or early Earth

habitats and present-day habitats has been bridged in two ways: assumptions aboutthe habitat or assumptions about life.

6.5.1Assumptions about the Habitat

Assumptions can be made about the physical and chemical characteristics of theearly Earth or the environment on the planet under study. The problem with thisapproach is that it can, without conscious effort, err on the side of biologicaloptimism, especially with respect to extraterrestrial environments.As an example, we can use nitrogen as a limiting nutrient. Nitrogen is essential

for the biosynthesis of proteins and nucleic acids. We know that nitrogen existed inthe environment of the early Earth, but we do not know in what biologicallyavailable form it occurred. Likewise for Mars, although the concentration of bio-logically available nitrogen in the Martian regolith is not known, there is nitrogenin the atmosphere. One might assume that this nitrogen could have been abioti-cally fixed into biologically available nitrogen compounds during the past history ofMars. However, without direct observation of nitrogen in the regolith, we empiri-cally do not know whether it exists, and therefore we cannot empirically assess thehabitability of Mars at present. As a result of these uncertainties there is atemptation to succumb to “biological optimism” (see Section 6.1), making extrap-olations from the particular environment being investigated that are most suited toproving life.

6.5.2Assumptions on Life

Theoretical life forms can be matched with the known or inferred conditions on theearly Earth or in the extraterrestrial environment. This method of bridging theastrobiological gap is the most pervasive in the literature. In the case of extra-terrestrial habitats, its inherent problem is the temptation to resort to “inventedphysiologies.”Because of a desire to show that the habitat can support life, new physiologies

with no counterparts on Earth are invented to show that life might be possible witha new innovation. The problem with this line of reasoning is that it requires atransgression from science into science fiction.

6.5.3Attempt to Formulate a Habitability Postulate

The purpose of a postulate for habitability is to bridge the gap between the knownand the hypothesized while attempting to reduce the chances of biological opti-

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mism. The principles are self-evident, but they need to be enunciated. One attemptto formulate a habitability postulate might be that derived of the following postu-late: “The proposition that a planet is or was habitable requires that the physio-logical requirements of microorganisms known at the time of assessment matchthe empirically determined combined physical and chemical conditions in theenvironment being assessed” (Cockell and Westall 2004).How does this simple postulate help to reduce biological optimism? First, we will

take the case of habitat assumptions. The second part of the postulate – “theempirically determined combined physical and chemical conditions in the environ-ment being assessed” – requires us to confine ourselves purely to direct observa-tions that have been made by spacecraft or from Earth. Thus, in the absence of ameasurement of biologically available nitrogen on the Martian surface, we mustconclude that we do not know whether Mars is presently habitable and we cannotknow this until we know the concentration of biologically available nitrogen. Thus,until such measurements are made, any hypothesis concerning the presence ofactive life on Mars must remain a biological speculation. The same is true formeasurements of all other known macro- and micronutrients required for life.Thus, the assessment of an extraterrestrial habitat as being conducive – or not, asthe case may be – for life requires the empirical measurement of all factors that arecurrently known to be critical to the kind of life being considered as a potentialinhabitant.The requirement to measure all the currently known nutrients in an extrater-

restrial or early Earth environment may be a little too stringent. In some particularcases, models might provide realistic insights. However, in the absence of totalknowledge of all physical and chemical parameters known to influence life, we areleft with gaps. For example, models used to assess the ultraviolet radiation environ-ment on Mars are an excellent example of where habitability has, at the time ofwriting, been assessed using models rather than direct field observations. In thiscase light penetration through a CO2 atmosphere is simple enough for us to beconfident that these models give realistic insights into the UV flux at the Martiansurface or on the early Earth, but even they must be treated with caution, as we donot know precisely the absorption properties of the ubiquitous Martian dust.How does the postulate help us to reduce biological optimism in the assump-

tions about life? The most parsimonious way to prevent biological optimism is notto make assumptions regarding the biochemistry and physiologies of extraterres-trial life and to use only those physiologies currently demonstrated to exist onEarth. This is required in the first part of the postulate – “requires that thephysiological requirements of microorganisms known at the time of assessment.”This seems intuitive, but in the case of Venusian exobiology, biological optimismhas been a pervasive problem, as we shall see in Section 6.6. Even if a postulatedphysiology appears to be thermodynamically possible, it does not necessarily meanthat it is biologically likely. There are costs and benefits to different modes of living.Thermodynamically plausible modes of existence in energy acquisition, motility,UV protection, etc., may not occur if there are some unknown biological orbiochemical reasons why such a physiology cannot exist. A possible example of

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such organisms is the hypothesis of thermosynthetic organisms that use temper-ature differences at the micron scale as a source of energy. These organisms seemthermodynamically possible, but they have never been observed on Earth. Theirexistence is therefore, by definition, science fiction at this time.Thus, using the above-suggested constraints, it is possible to bridge the astro-

biological gap in assessing the possibility of life on other planets and in habitats onearly Earth while at the same time minimizing the chances of falling prey tobiological optimism. If the postulate does not hold, the planet or the microenviron-ment is uninhabitable at the time of assessment.For the environment to become habitable, either

• new information about the extraterrestrial or early Earthenvironment must be obtained that brings the previouslyuninhabitable environment into the physical and chemicalhyperspace for life, or

• new organisms must be discovered on Earth that could po-tentially grow in the previously uninhabitable environment,i.e., new organisms must be discovered that fall within thephysical and chemical hyperspace defined by the extrater-restrial or early Earth environment under consideration.

6.6Some Test Cases for Habitability

It might be valuable to briefly look at two test cases of habitability. Aside fromapplying the postulate described above, they will also provide some additionalinformation on habitability.

6.6.1Test Case One: Life on Venus

The habitability of the clouds of Venus has been a matter of discussion in theexobiology community since the 1960 s. The clouds of Venus provide an example ofthe way in which exobiological thinking develops in favor of life, and they illustratethe potential value of a postulate on habitability. The life on Venus debate will bebriefly reviewed and the postulate of habitability will be applied as a test case.The habitability of Venus has been a matter of speculation since the turn of the

20th century. Arrhenius (1918) speculated that the planet was covered in micro-bially dominated swamps. Seckbach and Libby (1970) speculated that acidophilicalgae lived in hot Venusian oceans near the poles. Ichinose and Folsome (1973)also considered the habitability of Venus.These early speculations were afflicted by a lack of knowledge about the environ-

ment of Venus at that time and limited knowledge about the range of microbialphysiologies found on Earth. In the strictest sense, they do not conform to thesecond part of the postulate discussed here, because at the time of assessment it

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was known that microbes required nitrogen, phosphorus, liquid water, and a rangeof other macro- and micronutrients. Because there was no empirical knowledge ofthe abundance of such elements and compounds on Venus at the time of assess-ment, it was not possible to determine whether the physical and chemical environ-ment fitted the physiologies of organisms known on Earth at that time. Thus, “wedo not know if the planet is habitable, we require more measurement” would havebeen a stance consistent with the postulate discussed here.The conclusions of these scientists can be defended on the basis that models of

the environmental conditions on Venus at that time did support the potential forEarthlike organisms (the greenhouse effect on Venus had not been revealed), andso it was reasonable for them to infer that liquid water existed, and perhaps,knowing that Venus was rocky, other elements for life as well. These early authorsdid stay consistent with the first part of the postulate in that they used onlyorganisms empirically known on Earth. Arrhenius considered swamps, whileSeckbach and Libby were more specific and assessed Venus using the acidophilicalga Cyanidium caldarium, concluding that it could grow. In that sense they did notsuccumb to biological optimism in their assumptions about life.As models and observations of Venus improved, it became apparent that the

surface is not conducive to life. The temperature on the surface is almost globallyisothermal at 464 �C (see Chapter 8). This is at least 340 �C higher than thecurrently known upper temperature limit for life (Table 6.1, see also Chapter 5),and there is no liquid water on the surface. Because of this apparent hostility, theclouds of Venus then became a focus of astrobiological studies and have remainedso to this day.Morowitz and Sagan (1967) speculated on the existence of hydrogen-evolving

float bladders in the atmosphere of Venus. They proposed that these organismswould float through the Venusian cloud layer and would be 75 �m to 4 cm in size.This paper was the first suggestion of a life form for the Venusian clouds. Theproblem with the hydrogen-evolving float bladders is that they do not exist in thecloud deck of Earth, although there are marine organisms, e.g., most fishes and thenautiloids, that use buoyancy to regulate their position in the oceans of Earth andcyanobacteria that use gas vesicles for buoyancy. Hydrogen-evolving float bladdersmight seem thermodynamically plausible, but the lack of them on Earth forces us,under the conditions of the postulate proposed here, to reject them on Venus. Thepaper, although presenting a beautiful idea, tried to bridge the astrobiological gapby conceiving of entirely new organisms to fit the extraterrestrial environmentbeing considered, and thus it falls foul of the first part of the postulate.Since these early papers were written, a great deal of knowledge about the

Venusian cloud layer has been gathered. It contains sulfuric acid of concentrationsbetween and 81% and 98%. These concentrations present an extreme problem forosmoregulation in any putative cloud biota. Between 48 km and 55 km, thetemperature and pressure within the clouds are similar to ground conditions onEarth; however, Venus, with a maximum distance of 0.723 AU from the Sun, doesnot lie in the habitable zone of our Solar System (Fig. 6.2). The UV flux at the top ofthe cloud layer, because of Venus’s closer proximity to the Sun, is higher than on

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the surface of the Earth, although deeper in the clouds it is likely to be significantlyreduced by CO2 scattering and the presence of UV absorbers in the atmosphere.There are a number of ways around the sulfuric acid problem. One could

hypothesize the existence of microorganisms that can tolerate this high level ofsulfuric acid. However, the assumption of an entirely new physiology that has notbeen demonstrated on Earth requires a transgression into science fiction and is nottenable under the first part of the postulate.Another approach might be to assume that there are regions of the Venusian

clouds that do not have sulfuric acid and are long-lived. However, this has not beenempirically demonstrated at the time of this writing. Thus, this assumption wouldalso require a transgression into science fiction at the time of this writing, and it isnot tenable according to the second part of the postulate.Recently, the cloud deck was discussed as an abode for life (Cockell 1999). The

author concluded in a synthetic review that anaerobic sulfate-reducing chemo-autotrophic organisms fitted the habitat most closely on account of the presence ofsulfate as an electron acceptor, the presence of hydrogen as an electron donor, andthe abundance of carbon dioxide and other elements such as phosphorus andnitrogen in an essentially oxygen-free environment. But the paper did not suggestthat the organisms were actually there.More recently, there have been new proposals for organisms in the clouds of

Venus that consider new types of physiologies for growth and survival in the cloudlayer (e.g., Schulze-Makuch and Irwin 2002). Thus, the debate about life on Venuscontinues, and it illustrates the breadth of discussions in assessing the environ-ments of other planets and the potential value of a postulate.At the time of this writing (2006), what we empirically know about the cloud deck

of Venus is that there is sulfuric acid at concentrations between 81% and 98%suspended as droplets. We know there is very little water in the clouds. Onepositive observation for life that we can make is that temperatures and pressuresare favorable in certain regions. Because we do not know at the time of assessmentof any microorganism on Earth that naturally grows under these combined con-ditions in the aerosol state permanently in clouds, we should conclude, if we usethe postulate formulated above, that Venus is a dead world.This is not to say that Venus is a dead world but rather that at the time of

assessment – in other words, at the time this chapter was written – we mustconclude that it is a dead world.

6.6.2Test Case Two: Life on the Early Earth

The use of modern life on Earth as an analogy for ancient life has both positive andnegative aspects. Obviously, dinosaurs and the weird, but wonderful, Ediacaranfauna have no modern analogues. But what about single-celled organisms, such asbacteria?Using the theory of uniformity, i.e., “the present is the key to the past,”

propounded by the 18th century Scottish geologist James Hutton, the first obser-

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vations of microfossils in ancient rocks described microorganisms in the1.9-billion-year-old Gunflint Formation of Canada that resembled contemporarymicrobial mat and stromatolite-forming, oxygenic photosynthetic cyanobacteria.Since then, a plethora of investigations reported a wide variety of microfossils(often identified down to the species level), from increasingly older rocks up to thehighly metamorphosed, 3.8-billion-year-old Isua Greenstone Belt in southwestGreenland. In the latter case, cyanobacteria-like and even yeast-like species weredescribed. The well-preserved 3.5-billion-year-old chert horizons of the Barberton(South Africa) and Pilbara (northwest Australia) Greenstone Belts have yieldedmany species of cyanobacteria, as interpreted by Schopf, Walter, and others (seealso Chapter 1). The identification of these organisms stimulated a cycle of furtherstudies of modern cyanobacterial mats and the continued search for such organ-isms in the ancient rocks.The result of nearly 50 years of such investigations is the creation of a frame-

work of understanding and search methodology that is rigidly locked into theidentification of fossil cyanobacteria. Although cyanobacteria are wide ranging inmorphology, they tend to be much larger than most other types of bacteria andexhibit a type of cell differentiation that does not occur in other prokaryote groups.This makes them relatively easy to observe and identify with simple opticalmicroscopic methods. Moreover, their use of a more efficient energy-producingmetabolism led to

• a vast increase in biomass and• an important influence on the precipitation of calcium car-

bonate.

The prominent stromatolites so typical of the later Precambrian are a result ofthese two factors.Microbial mats formed by non-cyanobacterial microorganisms are, on the other

hand, subtler in terms of size, morphology, and volume importance. They, and themicroorganisms that form them, also require more sophisticated methods ofobservation, such as electron microscopes.The existence of cyanobacteria and yeasts in these ancient rocks would imply

very rapid evolution of life, because oxygenic photosynthesis is a sophisticatedmethod of obtaining energy, while the yeasts belong to the eukaryote group. Thisproduced a dichotomy regarding the environment of the early Earth, becausemodeling by the group of Kasting, as well as the geochemical analyses of the rocksused by Rye and coworkers (1995), suggested that the early environment was verypoor in oxygen. (On the contrary, Ohmoto [1999] contended that oxygen levels wereas high as they are today).The dichotomy can, however, be resolved very simply. It was shown by Westall

and Folk (2003), for example, that the yeast-like and cyanobacterial microfossilsfrom the Isua rocks are actually recent windblown or endolithic contaminants inthe cherts. With respect to the 3.5-billion-year-old cherts from Barberton and thePilbara, it has been suggested by Westall and coworkers and Brasier and coworkers(2002) that the fossil cyanobacteria are most likely artifacts. Westall (2003) dem-

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onstrated that, although life was relatively abundant in the Pilbara and Barbertoncherts, it consisted of small microorganisms that formed mats in non-oxygenicenvironments. These microfossils, with extremely rare exceptions, are individuallynot visible with the optical microscope, although the mats that they form are.Was the identification of cyanobacteria in the very ancient cherts biological

optimism? In fairness to the original interpretations, little was known about theenvironment of the early Earth, and thus the interpretation of oxygenic photo-synthesizers could be defended (the existence of sophisticated eukaryotes, such asyeasts, was rather surprising, however). The problems involved in studying themost ancient habitats on Earth have obvious relevance to the study of actual andancient habitats on other planets, such as Mars.

6.6.3R�sum� of the Two Test Cases

These two test cases show that the assessment of environments on other planets orthe early Earth as being habitable or uninhabitable needs a postulate that allows theenvironments and potential life to be evaluated with the minimum chance ofbiological optimism. Such a postulate was discussed in Section 6.5.The postulate suggests firstly that the physical and chemical conditions deter-

mined by direct or indirect analysis of rocks, in the case of ancient terrestrialenvironments, and by Earth or spacecraft observations, in the case of other planets,be used as a basis to evaluate the environment as an abode for life. Secondly, thephysiologies of known organisms should be used as a basis to assess the plausi-bility of a potential physiology capable of tolerating those conditions. When appliedto Venus, this postulate suggests that the planet is lifeless. With regard to the earlyEarth, it argues for new approaches to the interpretation of early life and ancientmicrofossils.In view of the increasing number of worlds coming under scrutiny and the

possibility that even the environmental conditions on the surface of Earthlikeextrasolar planets might one day be empirically determined, the debate about thedefinition of habitable and uninhabitable, and if habitable, by what type of life, hasbecome a useful one for standardizing approaches for the biological evaluation ofother planets.

6.7Conclusions

According to the postulate of habitability, the following items need to be considered:• Habitability is dependent upon the biochemical system under

consideration. However, assuming that life is carbon-basedand requires liquid water, sets of conditions required for lifecan be broadly defined and we can use these conditions toassess the habitability of other planets.

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• Conditions for habitability favor microorganisms because theyhave a broader range of environmental tolerances than mul-ticellular life and thereforemay bemore widespread, or at leastthe potential for their existence may be more widespread.

• Defining habitability and searching the Universe for itspresence (or demonstrating its absence) constitutes one of thegreat challenges of biology.

6.8Further Reading

6.8.1Books and Articles in Books

Arrhenius, S. (Ed.) The Destinies of the Stars,Putman, New York, 1918.

Cockell, C. S. Impossible Extinction – NaturalCatastrophes and the Supremacy of the Mi-crobial World, Cambridge University Press,Cambridge, 2003.

Crowe, M. J. The Extraterrestrial Life Debate,1750–1900, Dover Publications, 1999.

Dole, S. H.Habitable Planets for Man, Blaisdell,New York, 1964.

Haynie, D. T. Biological Thermodynamics,Cambridge University Press, Cambridge,2001.

Lowell, P. Mars as the abode of Life, 1909(reprinted 2005, Adamant Media Corpo-ration).

Lucretius The Nature of the Universe (Balti-more), 1951.

Marov, M., Grinspoon, D.H. The Planet Venus,Yale University Press, New Haven, 1998.

Robbins, E. I. Appelella Ferrifera, a PossibleNew Iron-Coated Microfossil in the IsuaIron-Formation, Southwestern Greenland,

in: Appel, P.W. U., LaBerge, G. L. (Eds.)Precambrian Iron Formations, Theophrastes,Athens, 1987, pp. 141–154.

Schopf, J.W. Tracing the Roots of the Univer-sal Tree of Life, in: A. Brack (Ed.) The Mo-lecular Origins of Life, Cambridge Univ.Press, Cambridge, 1998, pp. 336–362.

Schopf, J. W. Earth’s Earliest Biosphere: Statusof the Hunt, in: Eriksson, P. G. et al. (Eds.)The Precambrian Earth: Tempos and Events,Elsevier, Amsterdam, 2003, pp. 516–538.

Schopf, J.W., Walter, M. R. Archean Micro-fossils: New Evidence of Ancient Microbes,in: Schopf, J.W. (Ed.) Earth’s Earliest Bio-sphere, Princeton Univ. Press, Princeton,1983, pp. 214–239.

Westall, F. Precambrian geology and exobiol-ogy, in: Eriksson, P. G. et al. (Eds.), ThePrecambrian Earth: Tempos and Events,Elsevier, Amsterdam, 2003, pp. 575–586.

Wharton, D. Life at the Limits: Organisms inExtreme Environments, Cambridge Univer-sity Press, 2002.

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6.8.2Articles in Journals

Barghoorn, E. S., Tyler, S.A. Microorganismsfrom the Gunflint Chert, Science 1965, 147,563–577.

Beaumont, V., Robert, F. Nitrogen isotoperatios of kerogens in Precambrian cherts:a record of the evolution of atmosphericchemistry? Precambrian Res. 1999, 96,63–82.

Brasier, M. D., Green, O. R., Jephcoat, A. P.,Kleppe, A. K., van Kranendonk, M., Lindsay,J. F., Steele, A., Grassineau, N. Questioningthe evidence for Earth’s oldest fossils,Nature2002, 416, 76–81.

Caldeira, K. Continental-pelagic carbonatepartitioning and the global carbonate-silicatecycle, Geology 1991, 19, 204–206.

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Catling, D. C., Glein, C. R., Zahnle K. J., McKayC. P. Why O2 is required by complex life onhabitable planets and the concept of “oxy-genation time”, Astrobiology, 2005, 5, 415–438.

Cockell, C. S. Life on Venus, Planet Space Sci.1999, 47, 1487–1501.

Cockell, C. S. Astrobiology and the ethics of newscience, Interdiscipl. Sci. Rev. 2001, 26, 90–96.

Cockell, C. S., Westall, F. A postulate to assess“habitability”, Internat. J. Astrobio. 2004, 3,157–163.

Cockell, C. S., Catling, D., Davis, W. L., Kepner,R. N., Lee, P. C., Snook, K., McKay, C. P. Theultraviolet environment of Mars: biologicalimplications past, present and future, Icarus2000, 146, 343–359.

Cornford, F.M. Innumerable worlds in preso-cratic philosophy, Classic Quarterly 1934, 28,1–16.

Gilichinsky, D., Rivkina, E., Shcherbakova, V.,Laurinavichuis, K., Tiedje, J. Supercooledwater brines within permafrost – An un-known ecological niche for microorganisms:A model for astrobiology, Astrobiology 2003,3, 331–341.

Hoehler, T. M., Alperin, M. J., Albert, D. B.,Martens, C. S. Apparent minimum free en-ergy requirements for methanogenic Arch-aea and sulfate-reducing bacteria in an an-oxic marine sediment, FEMSMicrobiol. Ecol.2001, 38, 33–41.

Hoffman, P. F., Kaufman, A. J., Halverson,G. P., Schrag, D. P. A Neoproterozoic snow-ball earth, Science 1998, 281, 1342–1346.

Ichinose, N. K., Folsome, C. E. Lack of bacterialsurvival under cytherean-oriented condi-tions, Space Life Sciences 1973, 4, 332–334.

Joshi, M.M., Haberle, R.M., Reynolds, R. T.Simulations of the atmospheres of synchro-nously rotating terrestrial planets orbitingMdwarfs: Conditions for atmospheric collapseand the implications for habitability, Icarus1997, 129, 450–465.

Kashefi, K., Lovley, D. R. Extending the uppertemperature limit for life, Science 2003, 301,934.

Kasting, J. F. Earth’s early atmosphere, Science1993, 259, 920–926.

Kasting, J. F., Catling, D. Evolution of a habit-able planet, Ann. Re. Astron. Astrophys. 2003,41, 429–463.

Kasting, J. F., Whitmire, D. P.,Reynolds, R. T.Habitable zones around main sequencestars, Icarus 1993, 101, 108–128.

Kopp, R. E., Kirschvink, J. L., Hilburn, I. A.,Nash, C. Z. The paleoproterozoic snowballEarth: A climate disaster triggered by theevolution of oxygenic photosynthesis, Proc.Natl. Acad. Sci. USA 2005, 102, 11131–11136.

Kuhn, W. R., Atreya, S. K. Solar radiation in-cident on the Martian surface, J. Mol. Evol.1979, 14, 57–64.

Laskar, J., Joutel, F., Robutel, P. Stabilization ofthe Earth’s obliquity by the moon, Nature1993, 361, 615–617.

Lowell, R. P., DuBose, M. Hydrothermal sys-tems on Europa, Geophys. Res. Lett. 2005, 32,Art. No. L05202.

Malin, M. C., Edgett, K. S. Evidence for recentgroundwater seepage and surface runoff onMars, Science 2000, 288, 2330–2335.

Mancinelli, R. L. The search for nitrogen com-pounds on the surface of Mars, Adv. SpaceRes. 1996, 18, 241–248.

McKay, C. P., Toon, O. B., Kasting, J. F. Mak-ing Mars habitable, Nature 1991, 352, 489–496.

Melezhik, V. A. Multiple causes of Earth’searliest global glaciation, Terra Nova 2006,18, 130–137.

Morowitz, H., Sagan, C. Life in the clouds ofVenus, Nature 1967, 215, 1259–1260.

Muller, A.W. J. Finding extraterrestrial organ-isms living on thermosynthesis, Astrobiology2003, 3, 555–564.

Oder, R. K., Forsythe, J., Webber, D.M., Wells,J & Wells M. J. Activity levels of nautilus inthe wild, Nature 1993, 362, 626–628.

Ohmoto, H. Redox state of the Archean at-mosphere: Evidence from detrital heavyminerals in ca. 3250–2750 Ma sandstonesfrom the Pilbara craton, Australia: Com-ment, Geology 1999, 27, 1151–1152.

Orlando, T.M., McCord, T. B., Grieves, G. A.The chemical nature of Europa surface ma-terial and the relation to a subsurface ocean,Icarus 2005, 177, 528–533.

Patel, M. R., Berces, A., Kerekgyarto, T., Ronto,G., Lammer, H., Zarnecki, J. C. Annual solarexposure and biological effective dose rateson the Martian surface, Adv. Space Res. 2004,33, 1247–1252.

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Pimenov, N. V., Savvichev, A. S., Rusanov, I. I.,Lein, A. Y., Ivanov, M. V. Microbiologicalprocesses of the carbon and sulphur cycles atcold methane seeps of the North Atlantic,Microbiology 2000, 69, 709–720.

Pinti, D. L., Hashizume, K. 15N-depleted nitro-gen in Early Archean kerogens: clues onancient marine chemosynthetic-based eco-systems? Precamb. Res. 2001, 105, 85–88.

Pflug, H. D. Archean fossil finds resemblingyeasts, Geol. Palaeontol. 1979, 13, 1–8.

Pflug, H. D., Jaeschke-Boyer, H. Combinedstructural and chemical analysis of 3,800-Myr-old microfossils, Nature 1979, 280,483–486.

Rye, R., Kuo, P. H., Holland, H. D. Atmos-pheric carbon dioxide concentrations before2.2 billion years ago, Nature 1995, 378,603–605.

Schink, B. Energetics of syntrophic coopera-tion in methanogenic degradation, Micro-biol. Mol. Biol. Rev. 1997, 61, 262–280.

Schopf, J. W. Microfossils of the Early ArcheanApex Chert: new evidence of the antiquity oflife, Science 1993, 260, 640–646.

Schopf, J.W., Packer, B.M. Early Archean(3.3 billion to 3.5 billion-year-old) microfos-sils from Warawoona Group, Australia, Sci-ence 1987, 237, 70–73.

Schulze-Makuch, D., Irwin, L. N. Reassessingthe possibility of life on Venus: proposal foran astrobiology mission, Astrobiology 2002,2, 197–202.

Schulze-Makuch, D., Grinspoon, D.H., Abbas,O., Irwin, L. N., Bullock, M. A. A sulphur-based survival strategy for putative photo-trophic life in the Venusian atmosphere,Astrobiology 2004, 4, 11–18.

Seckbach, J., Libby, W. F. Vegetative life onVenus? Or investigations with algae which

grow under pure CO2 in hot acid media atelevated pressures, Space Life Sciences 1970,2, 121–143.

Takami, H., Inoue, A., Fuji, F., Horikoshi, K.Microbial flora in the deepest sea mud of theMariana Trench, FEMSMicrobiol. Lett. 1997,152, 279–285.

Walsby, A. E. Gas vesicles,Microbiol. Rev. 1994,58, 94–144.

Walsh, M.M. Microfossils and possible micro-fossils from the Early Archean OnverwachtGroup, Barberton Mountain Land, SouthAfrica, Precambrian Res. 1992, 54, 271–293.

Westall, F. The nature of fossil bacteria, J.Geophys. Res. 1999, 104, 16437–16451.

Westall, F. Gould S. J. Les procaryotes et leur�volution dans le contexte g�ologique, Pal�-ovol. 2003, 2, 485–501.

Westall, F., Folk., R. L. Exogenous carbona-ceous microstructures in Early Archaeancherts and BIFs from the Isua greenstonebelt: Implications for the search for life inancient rocks, Precambrian Res. 2003, 126,313–330.

Westall, F., Steele, A., Toporski, J. Walsh, M.,Allen, C., Guidry, S., Gibson, E., Mckay, D.,Chafetz, H. Polymeric substances and bio-films as biomarkers in terrestrial materials:Implications for extraterrestrial materials, J.Geophys. Res. 2000, 105, 24511–24527.

Westall, F., De Wit, M. J., Dann, J., Van DerGaast, S., De Ronde, C., Gerneke, D. EarlyArchaean fossil bacteria and biofilms in hy-drothermally-influenced, shallow watersediments, Barberton greenstone belt,South Africa, Precambrian Res. 2001, 106,93–116.

Whitman, W. B., Coleman, D. C., Wiebe, W. J.Prokaryotes: The unseen majority, Proc.Natl. Acad. Sci. USA 1998, 95, 6578–6583.

6.9Questions for Students

Question 6.1Describe two factors that might be important for the habitability of a planet. Why

are they important?Question 6.2Why is Jupiter’s moon Europa such a focus for astrobiologists? What factors

about this moon make it biologically interesting?

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Question 6.3Describe how the carbonate–silicate cycle is involved in regulating planetary

temperature.Question 6.4Discuss the assertion, “The circular objects on the moon are the fortresses that

lunarians have built to defend their cities.”

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7Astrodynamics and Technological Aspects of AstrobiologyMissions in Our Solar SystemStefanos Fasoulas and Tino Schmiel

The chapter gives an introduction into some basic technologicalaspects related to space missions in general and to astrobiologymissions to other planets, asteroids, comets, and/or moons inparticular. We focus on explaining the payload mass limits and thespecific constraints given by orbital mechanics.

7.1Introduction

Space missions are associated with many different applications, e.g., telecommu-nication, navigation, Earth observation, planetary exploration, and, very often,manned spaceflight. In the past few years, another discipline, namely, astrobiol-ogy, has become more and more important. Today, many scientific space missionsare especially dedicated to tackling astrobiological questions. The opportunities ofspace missions in low Earth orbit (LEO), by using space-based telescopes or byexploring in situ the planets (see Chapter 12), moons, and other bodies in our SolarSystem, provide unique possibilities for all scientists seeking a deeper understand-ing of the origin and nature of life. Thus, the community of scientists from otherdisciplines that formerly were not necessarily linked to the space sciences iscontinuously increasing.In the meanwhile, astrobiology missions are much diversified, using different

experiments in LEO, space-based telescopes, different landing probes, satellitesorbiting other planets, and, possibly in the very near future, sample return mis-sions from different locations in our Solar System. All these missions have theirspecific constraints, but they also have some common boundary conditions. There-fore, this chapter will concentrate on some selected basic boundary conditions forspace missions, especially for the reader who is not familiar with space engineer-ing. One main focus is to understand what space engineers mean when they talkabout a required velocity change ˜v to realize a particular mission, or about payload

7.1 Introduction 179

Complete Course in Astrobiology. Edited by Gerda Horneck and Petra RettbergCopyright � 2007 WILEY-VCH Verlag GmbH & Co. KGaA, WeinheimISBN: 978-3-527-40660-9

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and structure fractions, and why they are always worried about each gram of amission.Probably everyone has the feeling that the mass budget of a space mission is

critical, but why is this so? This shall be explained by the basic rocket equation.Then some basics of orbital mechanics will be discussed, followed by a briefintroduction into orbital maneuvers. Finally, in order to illustrate our generalfindings, missions to Mars will be briefly addressed.

7.2The Rocket Equation

7.2.1Single-staged Rockets

The original derivation of the rocket equation is attributed to Konstantin Tsiolkov-sky (1857–1935), a Russian schoolteacher (Fig. 7.1). The Tsiolkovsky rocket equa-tion, which is simply the result of the momentum conservation equation for asingle-staged rocket, states that the characteristic velocity change ˜vch of a rocket isproportional to the velocity of the exhaust gases ce multiplied with the logarithm ofthe initial total mass m0 divided by the final, end-of-burn mass mb:

˜vch ¼ ce lnm0

mb

� �(7.1),

where m0 ¼ mStructure þmPayload þmFuel (7.2),

and mb ¼ mStructure þmPayload (7.3).

The structure mass (mStructure) comprises the mass of all needed subsystems of arocket, e.g. the tanks, thrusters, pumps, pipes, sensors, and other subsystems. Thepayload mass (mPayload) essentially comprises the scientific instruments of a mis-sion plus all equipment supporting these instruments. Now, by defining a struc-ture mass ratio � and a payload mass ratio � according to

� ¼ mStructure

m0(7.4),

and � ¼mPayload

m0(7.5),

7 Astrodynamics and Technological Aspects of Astrobiology Missions in Our Solar System180

Fig. 7.1 Scheme for the derivation of the rocket equation;ce = velocity of the exhaust gas; vR(t) = velocity of the rocketdepending on time;mR(t) mass of the rocket depending on time.

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Eq. (1) can be rewritten as

˜vch ¼ ce ln1

�þ �

� �(7.6).

Table 7.1 shows that typical values for the structure fractions of chemical rocketsare below 10%. Based on this relation, Fig. 7.2 shows the resulting payloadfractions for different structure fractions as a function of ˜vch / ce. Now, in orderto illustrate the meaning of a structure fraction � = 5–10%, let us consider anexample from biology. What is the structure fraction of an egg, which means, whatis the shell mass related to the total egg mass?

Table 7.1 Initial total mass m0, structure fraction � for the firststage, and launch acceleration of three different rocket types(g0 = acceleration of gravity).

Rocket type Total mass m0 (kg) Launch acceleration Structure fraction �for the first stage

Scout 18 100 2.53 g0 8.9%Ariane 202 510 1.22 g0 6.6%Saturn V 2 850 000 1.19 g0 4.8%

In a non-representative experiment the author performed for a lecture in Dres-den, it turned out that the average structure fraction of six free-range eggs wasabout 11% of the total mass. Certainly, an eggshell is not made of the strongest

7.2 The Rocket Equation 181

Fig. 7.2 Payload fraction as a function of ˜vch / ce; see Eq. (6)(� = structure fraction; � = payload fraction).

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material that could be provided by nature, but, on the other hand, it usually doesnot have to withstand accelerations of up to several g’s, extreme vibrations, highinternal temperatures and pressures, aggressive and explosive fuel compounds,and so forth. This figurative example of an egg may give an impression of howthin and fragile rockets must be, having only about half the structure fraction ofan egg.Indeed, some rocket structures are so thin that they would buckle under their

own weight as soon as they are put upright. How is this done, then? First the fuel isput into the tanks under a higher pressure and then the rocket is put upright. Thetanks serve simultaneously as the skin structure of the rocket, and therefore theinternal fuel pressure stabilizes the rocket.As a matter of fact, the results of Eq. (6) as depicted in Fig. 7.2 show that, even for

a very ambitious structure fraction of about 5%, the characteristic velocity changewould be lower than 2.8 times the effective exhaust velocity if some payload, let’ssay of about 1% of the total mass, is assumed:

˜vch;max � 2:8 � ce for � ¼ 0:05 and � ¼ 0:01 (7.7).

The situation is of course worse for a higher structure fraction. On the other hand,the effective exhaust velocity ce depends on the total energy in the combustionchamber of a rocket, which is given for chemical rocket propellants mainly by theheat of formation ˜hR, e.g., for liquid hydrogen (LH2) and liquid oxygen (LOX) aspropellant, by

LH2 þ LOX ) H2Oþ ˜hR (7.8)

ce;max;ideal ¼ffiffiffiffiffiffiffiffiffiffiffi2˜hR

p(7.9).

Subsequently, the heat of formation must be chosen as high as possible in order toachieve a high exhaust velocity. Some values for chemical compounds with thehighest known heat of formation are given in Table 7.2. With the exception of thecompound BN, these compounds are oxides or fluorides of metals, hydrogen, orcarbon. The burning of metals in a combustion chamber is technically not an easytask, as they often build impermeable oxide layers that could prevent a completeburn or could block the nozzle throat. Some of them are extremely toxic and highlyreactive and thus are very difficult to store. Nevertheless, some metals as powders,mainly aluminum, are given as energy-increasing additions to solid rocket propel-lants. Thus, practically all chemical propellants used in rocketry are based onhydrogen and its compounds with carbon and nitrogen. Fluorine has neverreached an operational status because of its high reactivity. Thus, only oxygenand its compounds are used as oxidizers.

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Table 7.2 Heat of formation and maximum velocity of theexhaust gases [ce (max, ideal)] for some chemical compounds.

Compound Heat of formation(MJ kg–1)

Melting point( �C)

Boiling point( �C)

ce, max, ideal

(m s–1)

BeO 29.670 2 550 3 850 6 921LiF 23.606 848 1 767 6 869BeF2 21.495 547 1 170 6 554Li2O 19.986 1427 2 997 6 320B2O3 18.352 450 2 217 6 056AlF3 17.766 – 1 279 5 959MgF2 17.640 1263 1 357 5 937BF3 16.676 –129 –101 5 773Al2O3 16.425 2 045 2 700 5 729SiF4 15.000 –90 – 5 475MgO 14.958 2 642 2 800 5 468SiO2 14.623 1610 2 727 5 406HF 14.192 –85 19 5 326NaF 13.576 992 1 704 5 209H2O 13.442 0 100 5 183CF4 10.391 –184 –128 4 557BN 9.805 – (2 327) 4 427CO2 8.967 –58 –79[a] 4 233

a Sublimation point

Of course, the ideal value for the velocity of the exhaust gases ce cannot be reachedbecause of internal losses in the thrusters. When expanding the propellantsthrough a nozzle into a vacuum, for the hydrogen–oxygen combination a valueof about 4–4.5 km s–1 can be achieved, corresponding to an efficiency of about75%. Additionally, when launching from the ground, ce is further limited to about3–3.4 km s–1. Thus, one can calculate the ˜v limit for single-staged rockets to about9–10 km s–1. It will be shown later that this is the minimum value needed to get asatellite into a low Earth orbit.

7.2.2Multiple-staged Rockets

The solution to obtaining a higher ˜v, the staging concept, is based on the idea ofcontinuously jettisoning structure mass that is not needed anymore, e.g. thrusters,tanks, boosters, and payload fairing. The describing equation is then

˜vch;total ¼ ce1 lnm01

mb1

� �þ ce2 ln

m02

mb2

� �þ . . .¼

Xni¼1

cei lnm0i

mbi

� �(7.10),

where mbi 6¼ m0ðiþ1Þ (7.11).

7.2 The Rocket Equation 183

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Thus, the overall ˜v can be increased as depicted in Fig. 7.3. Indeed, ˜v could beincreased almost linearly with increasing number of stages. However, in this casethe payload fraction is decreased exponentially (notice that the payload fraction isdepicted on a logarithmic scale in Fig. 7.3). Thus, for multiple-staged rockets ˜v islimited if a payload fraction of at least 0.1% is assumed.

7.3Orbital Mechanics and Astrodynamics

7.3.1Some Historical Notes

The description of planetary motion has challenged scientists for many centuries.The early Greeks believed that celestial bodies moved in circles around the Earth.At that time this idea was in excellent agreement with observations for all distantstars. However, some of the observed bodies had a somewhat strange motion.Sometimes they moved backward and forward in the celestial sphere reference.Thus, they were called planets, from the Greek word for “wanderer” or “nomad.”This geocentric universe model probably reached its peak of refinement around the

7 Astrodynamics and Technological Aspects of Astrobiology Missions in Our Solar System184

Fig. 7.3 Payload fraction as a function of ˜vch for single- andmultiple-staged rockets; index in �i gives the number of stages,e.g., �1 for 1-stage rocket, �2 for 2-stage rocket, etc. The namesgive examples of different rockets launched.

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year 140 with Ptolemaeus (85–165), who calculated the orbits of the planets usingvarious combinations of circles known as epicycles.It took almost 1 500 years before Nicolaus Copernicus (1473–1543) placed the

Sun at the center of the Solar System, with the Earth rotating on its axis once a daywhile moving around the Sun once a year. However, Copernicus still believed thata planetary orbit should be circular, and his geometry was therefore as complex asthat of Ptolemaeus. It was Johannes Kepler (1571–1630) who, based on the preciseobservations of Tycho Brahe (1546–1601), discovered and formulated the laws ofplanetary motion that are known today as Kepler’s laws (Fig. 7.4).Kepler’s First Law: The planets orbit the Sun in elliptical orbits with the Sun at one

focus.Kepler’s Second Law: The line connecting a planet to the Sun sweeps out equal areas

in equal amounts of time.Kepler’s Third Law: The time required for a planet to orbit the Sun, called its period, is

proportional to the long axis of the ellipse raised to the 3/2 power.The constant of proportionality is the same for all the planets.

However, Kepler could not explain physically what forces were responsible forthese laws. This explanation was provided by Isaac Newton (1642–1727). Hepublished his three laws of motion and the law of universal gravitation in thePrincipia in 1687, stating the following:Newton’s First Law of Motion: A body stays at rest or moves with a constant

velocity on a straight line unless acted uponby an external unbalanced force.

Newton’s Second Law of Motion: An applied force is equal to the time rate ofchange of momentum.

Newton’s Third Law of Motion: All forces occur in pairs, and these two forcesare equal in magnitude and opposite in di-rection.

Newton’s Universal Law of Gravitation: The force of gravity between two bodies isdirectly proportional to the product of theirmasses and inversely proportional to thesquare of the distance between them.

7.3 Orbital Mechanics and Astrodynamics 185

Fig. 7.4 Illustration of Kepler’s laws.

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F ¼ ªmMr2

(7.12),

where F = force of gravity; m andM = mass of the two bodies; r = distance betweenthe two bodies; ª = gravitation constant.

ª ¼ 6:670 � 10�11 m3

kgs2(7.13).

These laws explain why a satellite, a moon, or a planet stays in orbit around theEarth, a planet, or the Sun, respectively. Very often it is argued that the gravitationalforce is counterbalanced by a centrifugal force. This is easy to understand but isphysically incorrect, because according to Newton’s first law of motion the bodyshould then maintain a constant velocity on a straight line, which is obviously notthe case.The correct answer is that gravity forces the satellite to fall towards the Earth;

however, because of its velocity it will never touch the Earth’s surface, meaning thatthe satellite is in a continuous free fall “around” the Earth. Today, it is known,thanks to Albert Einstein (1879–1955), that even this answer is not the completetruth. According to Einstein’s theory of relativity, the answer should be that gravitymass causes a curvature in space-time, in which the satellite is caused to move.By combining Newton’s second law of motion with his universal law of grav-

itation, an equation is obtained for the satellite’s acceleration vector €~r if it isassumed that gravity of only one central point mass is the only force:

€~r þ ªMr3

~r ¼~0 (7.14).

7 Astrodynamics and Technological Aspects of Astrobiology Missions in Our Solar System186

Fig. 7.5 Satellites can orbit a central mass inany of the four conic sections: circle, ellipse,parabola, or hyperbola.

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This equation is called the “two-body equation of motion,” giving the motion of asatellite’s position vector ~r in his orbit. A solution to this equation is the polarequation of a conic section:

r ¼ að1� e2Þ1þ ecos Ł

(7.15),

where a is the semi-major axis, e is the eccentricity, and Ł is the so-called trueanomaly, an angle measured from the closest point of the orbit to the currentposition (see also Fig. 7.4). A conic section is a curve formed by cutting a planethrough a right circular cone, as illustrated in Fig. 7.5. The angular orientation ofthe cutting plane determines whether the conic section is a circle, ellipse, parabola,or hyperbola.

7.3.2The Energy Conservation Equation

In order to illustrate the physical meaning of the possible orbits, another equationthat also can be derived from the two-body equation of motion can be used, the so-called “vis-viva” or “energy conservation equation”:

12v2

|fflfflffl{zfflfflffl}kineticenergy

� ªMr|fflfflfflfflfflfflffl{zfflfflfflfflfflfflffl}

potentialenergy

¼ const: ¼ � ¼ � ªM2a

¼ 12v21 (7.16),

where � is the total mass-specific mechanical energy of the satellite and v is themagnitude of the velocity. The term for the potential energy defines the potentialenergy as zero at infinity and negative at any radius less than infinity (Fig. 7.6).Using this definition, the specific mechanical energy of elliptical and circular orbitsis always negative, and a velocity at infinite distance to the central body masscannot be defined. As the energy increases and approaches zero, the semi-major

7.3 Orbital Mechanics and Astrodynamics 187

Fig. 7.6 Illustration of circular satellite orbits inEarth’s gravitation potential (note that these arenot orbits in physical space).

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axis of the ellipse gets larger and larger, approaching a parabolic orbit. The velocityon a parabolic orbit is thus high enough to escape from the central mass, having atinfinity a zero velocity relative to this mass. If the energy is further increased topositive values, the velocity is then high enough to escape from the central mass,having at infinity a finite velocity relative to this mass, leading to hyperbolic orbits.The orbit period P for elliptical orbits also can be derived from the energy

conservation equation as

P ¼ 2�

ffiffiffiffiffiffiffia3

ªM

s(7.17).

For circular orbits, the semi-major axis a simply equals the orbit radius r. (Recallthat this is just Kepler’s third law including the constant of proportionality.)

7.3.3Some Typical Velocities

The velocity of circular orbits is given by the energy conservation equation as

vcircle ¼ffiffiffiffiffiffiffiªMr

r(7.18).

Therefore, the velocity needed to maintain a circular orbit is higher the closer thesatellite is to the central body. This is illustrated in Fig. 7.6. Notice that the curvesshown in Fig. 7.6 are not orbits in physical space but only in potential energy.The velocity on elliptical, parabolic, or hyperbolic orbits at a certain distance from

the central mass can be calculated by

7 Astrodynamics and Technological Aspects of Astrobiology Missions in Our Solar System188

Fig. 7.7 Illustration of an elliptical satelliteorbit in Earth’s gravitation potential (note thatthis is not an orbit in physical space).

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v ¼ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi2ªMr

� ªMa

r(7.19).

Thus, the velocity reaches a maximum value for the closest orbit point and aminimum for the most distant point of the orbit (Fig. 7.7).Now, staying on Earth’s surface, what kind of orbits can be achieved and what

velocities are needed? Assuming a launch location on a big mountain and that theEarth is a perfect sphere without an atmosphere, the velocity to which a satellitemust be accelerated perpendicular to Earth’s gravitational field is simply

vLowEarthOrbit ¼ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiªMEarth

REarth

r� 7:91

kms

(7.20).

This value is known as the first cosmic velocity. For slightly lower values, thesatellite would fall in an elliptical trajectory back to Earth; for higher values it wouldreach an elliptical orbit around the Earth. However, if the velocity is furtherincreased, reaching an infinite value for the semi-major axis a, then the satellitewould be on a parabola. The velocity needed for this at Earth’s surface is called thesecond cosmic velocity and has a value of

vParabola ¼ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi2ªMEarth

REarth

r� 11:2

kms

(7.21).

Figure 7.8 depicts these findings. If losses resulting from atmospheric drag or fromthe fact that satellites cannot be launched directly perpendicular to Earth’s gravita-tional field are taken into account, about 15–20% must be added in order to

7.3 Orbital Mechanics and Astrodynamics 189

Fig. 7.8 Illustration of velocities needed forreaching a LEO and for escaping from thegravitational pull, assuming that Earth is aperfect sphere without atmosphere (and thatthe pitcher has enough thrust). See text formore details on the required velocities for thedifferent orbits.

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estimate the necessary ˜v to get a satellite into orbit. Thus, for low Earth orbits, this˜v demand is about 9–10 km s–1. Figure 7.8 also illustrates that for establishingelliptical orbits other than those going through the launching point, additionalmaneuvers or burns are necessary.

7.4Orbital Maneuvers

7.4.1High-thrust Maneuvers

To change a satellite’s orbit, its velocity vector in magnitude and/or direction mustbe changed. Compared to the orbital period, most chemical propulsion systemsoperate for a short time only, so the maneuver can be treated as an impulsivechange in velocity while the position is the same. Therefore, any maneuver mustoccur at a point where the old orbit intersects with the new. If there is nointersection, then an intermediate orbit must be used, which intersects both.Generally, the change in velocity needed to go from one orbit to another is

~̃v ¼~v2 �~v1 (7.22).

As a first example, an orbit change from an Earth equatorial orbit to a polar orbit atthe same altitude is considered. The required velocity change would be

j ~̃v j ¼ j~v2 �~v1j ¼ffiffiffi2

pv1 (7.23).

7 Astrodynamics and Technological Aspects of Astrobiology Missions in Our Solar System190

Fig. 7.9 The Hohmann transfer ellipse between two circularorbits. Note that the velocity on the final orbit 2 is lower than onthe initial orbit 1, but the satellite must be accelerated twice forthe transfer.

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Performing this maneuver in low Earth orbit would mean that the required ˜v isffiffiffi2

pv1 � 7:91 km s�1 ¼ 11:2 kms�1. Recall that this is just the value required to

escape from Earth’s gravitation when launched from the ground! Out-of-orbital-plane changes are therefore performed only when absolutely required.In order to establish an orbit that is higher in altitude (e.g., a geosynchronous orbit

[GEO]) than the initial one (e.g., a LEO), another typical maneuver is performed. Themost efficient direct transfer orbit is an ellipse that tangentially intersects both orbits(Fig. 7.9). This transfer ellipse is called theHohmann transfer orbit. The total changein velocity required for the transfer is the sum of the velocity changes at the perigeeand apogee of the transfer ellipse. Because the velocity vectors are collinear, thevelocity changes are simply the differences in magnitudes of the velocities in eachorbit, namely, for circular initial and final orbits:

˜vHohmann ¼ ˜v1 þ ˜v2 ¼ vellipse;1 � vcircle;1� �

þ vcircle;2 � vellipse;2� �

(7.24).

The result of Eq. (24) is depicted in Fig. 7.10 as a function of different ratios of theinitial and final radii. An important and somewhat surprising result is that therequired ˜v for a transfer between two circular orbits around the same central massreaches values above the required˜v for escaping fromgravitational attraction. This is,for example, the case for a transfer between LEO (rLEO » 6 600 km) and GEO(rGEO » 42 000 km). The reason for this is that at the first burn the fuel mass neededfor the second burn has to be accelerated and lifted in the gravitational field. Thus,from an energetic point of view, it is less expensive to launch a satellite from LEO intoan interplanetary orbit than to GEO. Finally, in most cases it turns out that therequired˜v for an orbit change is higher themoremaneuvers (burns) are performed.

7.4 Orbital Maneuvers 191

Fig. 7.10 Required ˜v for a Hohmann transfer ellipse betweentwo circular orbits.

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7.4.2Low-thrust Maneuvers

It is often argued that thrusters such as electrical or ion thrusters can achieve amuch higher exhaust velocity, and therefore a higher overall velocity change ˜v,than chemical rockets. This is in many cases true, although the structure fractionwould certainly be increased because of the needed additional power support.However, the total thrust achieved is usually not sufficient to allow for an appli-cation in the first stages of a rocket. Nevertheless, when using electrical thrusters,e.g. as a third stage, the total ˜v can be increased as depicted in Fig. 7.11.On the other hand, because of the low thrust, the operation time is also

increased, leading to the situation of having an almost infinite amount of smallpulses (as approximation for a continuous long-term burn). Considering thediscussion of the previous chapter, this would lead to an increase of the required˜v to accomplish the same orbit transfer. As an example, Fig. 7.12 shows the resultfor a transfer between two circular Earth orbits in comparison to the Hohmanntransfer. Thus, it is important to have not only a high ˜v capability of a rocket butalso a low ˜v requirement according to the orbit maneuvers that are possible withthe used propulsion systems. An overview of the required ˜v to accomplish acertain mission is given in Table 7.3.

7 Astrodynamics and Technological Aspects of Astrobiology Missions in Our Solar System192

Fig. 7.11 Payload fraction as function of ˜v for multiple stagedrockets. Different combinations of chemical and electrical propul-sion are compared. Note that electrical thrusters have higher ex-haust velocity than chemical thrusters and that generally �chemical

< �electrical and ce,chemical < ce,electrical, but the thrust Felectrical << Fchemical.

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Table 7.3 Typical ˜v requirement and resulting typical payloadfraction � for different mission types.

Mission type ˜v (km s–1) �

LEO �9–9.5 0.04Escape from Earth’s gravitation �12.5 0.015LEO + Hohmann transfer to GEO �13 0.01Earth–Moon–Earth �18 0.0025Grande tour (Earth–Jupiter–Saturn–Uranus–Pluto) �23 0.00035Earth–Mars–Earth �23 0.00025Comet rendezvous �25 0.0002Mission out of ecliptic plane (35 �) �26 0.00016Earth–Mars–Earth with “soft” landing �34 0.00001Crash into Sun �40 0.000005

LEO = Low Earth orbitGEO = Geosynchronous Earth orbit

7.4.3Gravity-assist Maneuvers

Table 7.3 illustrates that the ˜v requirements for space missions are very high, andtherefore – according to the Tsiolkovsky equation – the resulting payload fractionsare very low. This is especially the case for interplanetary missions to the outerplanets of our Solar System.

7.4 Orbital Maneuvers 193

Fig. 7.12 Comparison of the ˜v requirement for a Hohmanntransfer and a transfer with continuous low thrust.

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Fortunately, there is an alternative that allows for increasing a vehicle’s energy(and therefore velocity) relative to the Sun without requiring fuel: the “gravity-assist” or “swing-by” maneuver. This maneuver uses a planet’s gravitational fieldand orbital velocity to “sling” the satellite, changing its velocity in magnitude anddirection (Fig. 7.13). As the satellite enters the gravitational field on a hyperbolicorbit and passes behind the planet, the planet pulls it in the direction of the planet’smotion. Thus, it gains energy with respect to the Sun, altering the satellite’soriginal orbit around the Sun. If the satellite passes in front of a planet, it is pulledin the opposite direction, causing a slowdown in velocity relative to the Sun. Ofcourse, because of Newton’s laws (action – reaction) the same energy changeoccurs for the planet as well. However, because of the significantly smaller massof the satellite, the effect on the satellite can be extreme, whereas for the planet it isnegligible.Gravity-assist trajectories often make the difference between possible and im-

possible missions. For example, the Galileo mission to Jupiter was launchedtowards the inner Solar System, performing first one swing-by maneuver at Venusfollowed by two subsequent swing-by maneuvers at Earth. Another example is theUlysses probe, which performed a gravity-assist maneuver at Jupiter that sent it outof the ecliptic plane into a polar orbit around the Sun.Of course, in order to establish such maneuvers, the constellation between the

Earth, the gravity-assist planet, and the target planet must be in accordance. This

7 Astrodynamics and Technological Aspects of Astrobiology Missions in Our Solar System194

Fig. 7.13 Illustration of gravity-assist maneuvers. Left: in aheliocentric reference system, right: in a topocentric (planet)reference system.

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often determines possible “launch windows,” meaning the time frame in whichthe spacecraft has to be launched.Finally, it is important to note that in both cases, either acceleration or deceler-

ation of the satellite relative to the Sun, it leaves the planet’s sphere of influence ona hyperbolic orbit (relative to the planet!). Thus, in order to establish an orbitaround a planet, an impulse (thrust), and therefore fuel, is again required.

7.5Example: Missions to Mars

In the following sections, some of the general findings from the previous chapterswill be discussed regarding missions to our neighboring planet Mars. First, in orderto establish an interplanetary trajectory to Mars, the satellite should be launchedwith a velocity higher than 11.2 km s–1 (the escape velocity from the Earth) relative toEarth. Further, it should be launched in the direction of the Earth’s motion aroundthe Sun; otherwise, the ˜v requirement would be increased by the Earth’s ownvelocity around the Sun of about 29.8 km s–1. For a launch to Mars, often the Earth’sown rotational velocity is also used, i.e., a launch towards the east and additionallyduring nighttime is performed (assuming a direct launch from Earth’s surface andan injection into a Hohmann transfer). As already discussed, the most energy-efficient transfer trajectory is a Hohmann transfer joining Earth and Mars’ orbitaround the Sun. Of course, as soon as the satellite’s orbit intersects with the Martianorbit, the planet should be at this position in order to set up a “rendezvous.” A certaininitial constellation between the two planets is therefore needed, as seen in Fig. 7.14.

7.5 Example: Missions to Mars 195

Fig. 7.14 Launch window for a mission to Mars.

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All these issues define the launch window, which opens for just a few days or weeksand is additionally restricted in local time. If the window is missed, the nextopportunity occurs after about 780 days.Because of the limited payload fraction of the launch vehicle, the amount of fuel

carried with the probe is limited, too. Thus, only a few minor interplanetarycorrection maneuvers (usually about four or five) are possible in order to adjustthe orbit for a typical journey of about 500 000 000 km. Themain fuel portion is thenneeded to slow down the spacecraft to a mostly high eccentric orbit around Mars,except, of course, if a direct landing without a prior velocity change is planned.Many of the orbital missions to Mars performed in the last few years make use of

so-called “aerobraking” maneuvers to establish a final orbit. Therefore, the closestpoint (periapsis) to the planet is chosen so that the spacecraft flies through theupper part of the atmosphere, which causes aerodynamic drag and further slowsdown the spacecraft, and subsequently its apoapsis (most distant orbital point). Theeffect on the apoapsis is higher than that on the periapsis, and after performingthis aerodynamic break over several passages, an orbit with a lower eccentricity isachieved. Finally, a small burn at the apoapsis lifts the periapsis out of theatmosphere and the final orbit is established.Again, the necessary fuel mass for the braking maneuvers together with the

required satellite system mass, (e.g., energy, attitude, and orbit control; commu-nication; thrusters; tanks), significantly limits scientific instrument mass. Thesituation is similar for entry and landing probes where some of the fuel necessaryfor orbit insertion can be saved, but additional system mass must be introduced,e.g., for the heat shield.Because the scientific payload for interplanetary missions is so restricted in mass

(and also in energy demand), an alternative to studying the planets or their surfacematerial is to bring material from other celestial bodies, especially from Mars, toEarth for further in-depth investigations. Therefore, some basic boundary condi-tions and scenarios for a Mars sample return (MSR) mission will be discussed here(see Figs. 7.15 to 7.17). A more detailed discussion is provided by D. Boden and S.Hoffmann in Human Spaceflight: Mission Analysis and Design, edited by W. Larsonand L. Pranke (1999).The first part of anMSRmission, the way toMars on aminimum energy transfer,

has already been discussed. Assume that the spacecraft is already in aMars orbit andis supplied with somematerial from the Mars surface that has been collected by useof a landing probe. Similar to the outbound part, it has to wait until the constellationbetween Mars and Earth allows for a return flight trajectory. For low-energy trans-fers, the Mars stay-time may reach values of more than one Earth year. Adding thetransfer times, the total mission duration lasts for more than 2.5 years. The required˜v for the return injection is lower than for the trans-Mars injection; however, onehas to recall that with current technologies the necessary fuel mass must beimported to Mars. As shown in Fig. 7.15, for the low-energy transfer from a LEOto a Mars orbit and a direct flight back to Earth, a ˜v of about 8.2 km s–1 is needed.The ˜v needed for a launch from Earth, the ˜v for a launch from the Mars surface(about 4 km s–1), and the ˜v for any rendezvous or trajectory correction maneuvers

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must be added to this value. Thus, even assuming a direct landing upon Earthreturn, which is extremely challenging because of the high return velocity, theoverall ˜v needed for such a mission is in the best case about 20 km s–1. Thishigh overall˜v value yields extremely low payload fractions, which could be returnedto Earth (including the transfer vehicle with heat shield and other items).Using fast, high-thrust transfers as depicted in Fig. 7.16 is not really an alter-

native for reducing the overall mission time, because the waiting time for the

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Fig. 7.15 Typical low-energy scenario (Hohmann transfer) for anMSR mission.

Fig. 7.16 Typical scenario for a short transit time for an MSRmission.

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return launch window is enlarged. Thus, only a small amount of the return flighttime can be saved. However, the required ˜v is dramatically increased, easilyreaching values above 25 km s–1.What about using gravity-assist maneuvers? This possibility exists, as illustrated

in Fig. 7.17. The alternative of performing a swing-by maneuver at Venus couldshorten the overall mission time, while the total ˜v requirement would be muchlower than the high-thrust transfer, but nevertheless higher than a double low-energy Hohmann transfer (Fig. 7.15). However, the spacecraft would fly closer tothe Sun than the orbit of Venus, which subsequently has an impact on the overalldesign, and especially on the thermal control system because of the higher solarradiation.From this brief discussion of potential Mars sample return mission scenarios it

becomes obvious that orbital mechanics provide a variety of possibilities. However,it is also obvious that generally only very small payload fractions can be realized andthat each scenario has some specific benefits and drawbacks. In addition, techno-logical issues not addressed here in detail must be taken into account, such aspower supply, data processing, and communication requirements; automatedguidance; navigation and control; system autonomy; entry, descent, and landingtechnologies; robotics and mechanisms; propulsion, etc. Thus, the payload massused to calculate the payload mass ratio of a rocket (see Section 7.2) includes allspacecraft subsystems that are needed for survival and control of the sciencepayload. Table 7.4 gives an overview of the subsystems of a spacecraft that arerequired to service the science payload.Finally, for potential biological payloads, planetary protection requirements, as

discussed in Chapter 13, must be added, making the situation even more complexand challenging, but not unsolvable.

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Fig. 7.17 Scenario for an MSR mission using a Venusgravity-assist maneuver for return.

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Table 7.4 Overview of typical spacecraft subsystems forservicing scientific payloads (e.g., scientific instruments).

Spacecraft system Subsystems of spacecraft system

Electrical power system (EPS) Electrical power generationConditioning, storage, and supply (e.g., solargenerators, batteries, fuel cells, radio isotopegenerators, power control units)Electrical power regulation and distribution

Structure and mechanism system (SMS) Carrying shock and vibration loads associated withacceleration during ground operation, launch,in-orbit operations, re-entry and landingHolding of payload, electronics, sensors, antennas,etc., in stable positionsProtection against influences from space environ-ment

Thermal control system (TCS) Temperature control for all spacecraft components,e.g., batteries, electronics, propellant tanks, sen-sors, actuators, solar arrays, structures, etc.Passive thermal control systems via heat conduc-tion and radiation, e.g., radiators, coatings, multi-layer insulation (MLI), heat sinks, joint fillers, etc.Active thermal control systems, e.g., heat switches,active radiators, heat pipes, single- and two-phasefluid loops, electrical heaters, etc.

Communication system (CS) Transmitters and receivers or transpondersAntenna systems and antenna pointingSignal-to-carrier frequency modulation and multi-plexing, signal demodulation, etc.

Command and data handling (C&DH) Payload data processing and recordingHousekeeping and science data encoding andtelemetryError handlingSignal decoding and telecommand handling anddistribution to the appropriate devicesSoftware and computer systems

Propulsion system (PS) Thrusters (chemical, electrical) for launch, in-orbitinsertion, orbit transfer, orbit and attitude mainte-nance, reentry and landing maneuvering, attitudecontrol, etc.Fuel and oxidizer storage and handling

Attitude and orbit control system (AOCS) Orbit determination and controlAttitude determination and control = spacecraftstabilization in desired directions despite thedisturbance torques, uses sensors and actuators(e.g., star trackers, sun sensors, magnetic actuators,momentum wheels, fly wheels, thrusters, etc.)

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7.6Further Reading

Anderson, J. D. Introduction to Flight, McGraw-Hill Inc., 1989.

Buedeler, W. Geschichte der Raumfahrt, SiglochEdition, 1982.

Brown, C. D., Spacecraft Mission Design, AIAAEducation Series, Washington D. C. 1992.

Dadieu, A., Damm, R., Schmidt, E.W. Rake-tentreibstoffe, Springer Verlag, 1998.

Griffin, M. D., French, J. R. Space Vehicle De-sign, AIAA Education Series, WashingtonD. C. 1991.

Hammond, W.-E., Space Transportation: A Sys-tems Approach to Analysis and Design, AIAAEducation Series, Washington D. C. 1999.

Humble, R.W., Henry, G. N. and Larson, W. J.Space Propulsion Analysis and Design, SpaceTechnologies Series, McGraw Hill, 1995.

Larsen, W. J., Pranke, L. K. (Eds.) HumanSpaceflight: Mission Analysis and Design, SpaceTechnology Series, McGraw Hill, 1999.

Messerschmid, E., Fasoulas, S. Raumfahrtsys-teme, Springer, Berlin, 2004.

Oberth, H. Die Rakete zu den Planetenr�umen,R. Oldenbourg, M�nchen, 1923, 5th editionUNI–Verlag Dr. Roth-Oberth, Feucht, 1984.

Sellers, J. J. et al. Understanding Space – anIntroduction to Astronautics, McGraw-HillEducation, 2000.

Sutton, G. P. Rocket Propulsion Elements – AnIntroduction to the Engineering of Rockets,John Wiley and Sons, Inc., New York, 1992.

Vallado, D. A., McClain, W. D. Fundamentals ofAstrodynamics and Applications, Kluwer Aca-demic Publishers, 2001.

Wertz, J. R., Larson, W. J. (Eds.) Space MissionAnalysis and Design, 2nd edition, KluwerAcademic Publishers, 1999.

7.7Questions for Students

Question 7.1Why is the ˜vch capability of a single-staged rocket limited?Question 7.2What is the basic idea behind the “multi-stage” concept?Question 7.3Why is the ˜v needed for a Hohmann orbit transfer from a low earth orbit to a

geostationary orbit higher than the ˜v needed to escape from Earth’s gravitationalfield from low earth orbit?Question 7.4Why is it practically impossible to use electrical thrusters in the first stage of a

rocket?Question 7.5Planetary gravity-assist maneuvers are usually performed in order to increase a

spacecraft’s velocity (energy) relative to the Sun. (a) Where does this energy comefrom? (b) Do you think that it is also possible to decrease the velocity relative to theSun? If yes, how would you perform the maneuver?Question 7.6What fuel mass is needed in order to accelerate a mass of 200 kg (payload,

structure, and motor mass) with a single-stage rocket (in a force-free environment)from zero to the triple exhaust velocity (3 ce)?

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Question 7.7Calculate the orbit velocities and orbit periods of circular Earth orbits with the

following altitudes H above the Earth’s surface:H = r – R0 = 200 km;, 500 km, 1 000 km, or 10 000 kmWhat altitude would be needed for a geostationary satellite (note that a sidereal

day is slightly smaller than 24 h, namely 23 h, 56 min, 4 s)?Note:Earth mass ME = 5.974 � 1024 kgGravitational parameter: ªME = 3.986 � 1014 m3 s–2

Earth radius R0 = 6.378 � 106 mQuestion 7.8An unmanned spacecraft has been placed in a 500-km circular orbit around the

Earth. (a) Calculate the ˜v budget needed for a Hohmann transfer from this orbitto a 600-km circular orbit in which a docking maneuver with a satellite could takeplace. (b) Calculate the necessary relative phase angle between the two spacecraft atthe time of injection into the Hohmann transfer ellipse so that the dockingmaneuver can take place at the same time as the spacecraft reaches the final orbit.Notice that the transfer time of the Hohmann transfer is simply half of the orbitalperiod for this orbit. (c) How much time will pass between two possible constella-tions?Question 7.9Discuss some of the requirements coming from a scientific payload that have

influences on the design of the spacecraft subsystems listed in Table 7.4.Question 7.10Imagine that a potential scientific payload needs two times more electrical power

than a competitive, but not so sophisticated, payload. What influences will occur tothe design of the electrical power system (EPS), the thermal control system (TCS),the structure and mechanism system (SMS), and the attitude and orbit controlsystem (AOCS)?

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8Astrobiology of the Terrestrial Planets, with Emphasis on MarsMonica M. Grady

The planets of particular relevance to this chapter are the four rockyplanets in the innermost region of the Solar System: Mercury,Venus, Earth, and Mars. Each of these planets has the potential, toa greater or lesser extent, to host life; in the case of Earth, thispotential appears to have been fully realized. In this chapter thesefour rocky planets are examined and the relative likelihood of lifeevolving on Mercury, Venus, and Mars is assessed. Most emphasiswill be placed on Mars because, after Earth, it seems to have thehighest potential to host life. Besides observations by telescope andspacecraft, Martian meteorites are discussed as an additional wayof exploring Mars.

8.1The Solar System

Our Sun and its planetary system are located approximately two-thirds of the wayout along one of the arms of the (approximately 10–12 billion years old) Milky Wayspiral galaxy. The Sun is sometimes described as an undistinguished star in anundistinguished neighborhood – it is a G class star surrounded by its family ofplanets and their satellites, plus asteroids and comets. Advances in understandingthe processes that led to the formation of the Sun and Solar System have resultedfrom astronomical observations of star formation regions in molecular clouds andthe recognition and observation of protoplanetary disks and planetary systemsaround other stars (see Chapter 2). If we wish to understand the processes by whichlife arose and became established on Earth, and whether there are possiblelocations beyond Earth where life might exist, then it is also necessary to under-stand the starting materials and processes that led to the formation of the SolarSystem.The first stage in the history of the Solar System was the collapse of an

interstellar cloud: gravitational instability within the cloud resulted in collapse ofa fragment of the molecular cloud to form a protoplanetary disk, or solar nebula.

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The mechanism that triggered cloud collapse is not clear. Several possibilities havebeen suggested. Examples include a shock wave from a nearby supernova or theejection of a planetary nebula from a giant star; but whatever the mechanism, thecollapse of the cloud and subsequent accretion of material must have taken placeover a relatively short time interval, around 1–3 million years, as deduced bymeasurements on meteorites. As the cloud fragment collapsed, dust grains felltowards the center of the nebula, clumping together to form increasingly largebodies. The growth of planet-sized bodies from micron-sized dust grains wascontrolled by several factors, such as the nature of the initial grains – whetherfluffy or compact – and the degree of turbulence within the nebula. End-membermodels for planetesimal (small planet) formation include coagulation of materialby gravitational instability in a quiescent nebula or coagulation during descent tothe midplane of a turbulent nebula. The aggregation of interstellar dust (£ 0.1 �min diameter), eventually forming kilometer-sized planetesimals and culminating inthe asteroids and planets, took less than 30 million years following formation of thefirst solid materials.The inner, rocky terrestrial planets (i.e., Mercury, Venus, Earth, and Mars; Table

8.1), formed sufficiently close to the proto-Sun that volatile elements were lostthrough vaporization and water did not condense to ice. Marking the boundarybetween the rocky planets and the outer gas giants is the asteroid belt. Theasteroids are a swarm of several thousand planetesimals, the largest of which,Ceres, is about 1 000 km across; most asteroids are on the order of a few kilometersacross.

Table 8.1 Properties of the terrestrial planets and the Moon.

Property Planet

Mercury Venus Earth Moon Mars

Mass (1024 kg) 0.330 4.87 5.97 0.073 0.642Diameter (km) 4879 12 104 12 756 3475 6794Density (kg m–3) 5427 5243 5515 3340 3933Gravity (m s–2) 3.7 8.9 9.8 1.6 3.7Escape velocity (km s–1) 4.3 10.4 11.2 2.4 5.0Rotation period (h) 1407.6 –5832.5[a] 23.9 655.7 24.6Length of day (h) 4222.6 2802.0 24.0 708.7 24.7Distance from Sun (106 km) 57.9 108.2 149.6 0.384[b] 227.9Perihelion (106 km) 46.0 107.5 147.1 0.363[b] 206.6Aphelion (106 km) 69.8 108.9 152.1 0.406[b] 249.2Orbital period (days) 88.0 224.7 365.2 27.3 687.0Orbital velocity (km s–1) 47.9 35.0 29.8 1.0 24.1Orbital inclination (degrees) 7.0 3.4 0.0 5.1 1.9Orbital eccentricity 0.205 0.007 0.017 0.055 0.094

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Property Planet

Mercury Venus Earth Moon Mars

Axial tilt (degrees) 0.01 177.4 23.5 6.7 25.2Mean temperature ( �C) 167 464 15 –20 –65Surface pressure (105 Pa) 0 92 1 0 0.01Number of moons 0 0 1 0 2Global magnetic field? Yes No Yes No No

Source: NASA planetary fact sheet (http://nssdc.gsfc.nasa.gov/planetary/factsheet/index.html)a Negative numbers indicate retrograde (backwards relative to the Earth) rotation.b Values represent mean apogee and perigee for the lunar orbit. The orbit changes over the

course of the year, so the distance from the Moon to Earth ranges roughly from 357 000 kmto 407 000 km.

The sequence of events that produced the innermost rocky planets from theprotoplanetary disk also produced planets of an entirely different nature: thegas giants Jupiter, Saturn, Uranus, and Neptune. These planets probably startedout in the same way as the terrestrial planets, as an accumulation of rockymaterial. Temperatures at this distance from the proto-Sun were sufficientlylow that water ice would also accrete along with the dust; volatile elements wouldalso be retained and not vaporized. Runaway accretion resulted in central coresthat were sufficiently large to attract and retain significant masses of hydrogen(H) and helium (He) from the remaining nebula gas. Uranus and Neptune,however, have lower H and He and higher carbon (C), nitrogen (N), and oxygen(O) abundances than Jupiter and Saturn. It is thought that this indicates thatUranus and Neptune formed some time after Jupiter and Saturn, after the nebulagas had dissipated.Beyond the giant planets lies Pluto, the smallest planet in the Solar System, with

a radius even smaller than that of the Moon. Beyond Pluto, at 30–50 astronomicalunits (AU), is the Kuiper Belt, an accumulation of rocky and icy bodies more akinto comets than asteroids. Pluto, indeed, may be a Kuiper Belt Object, rather than aplanet. At the outermost reaches of the Solar System, in fact defining the boundaryof the Solar System, is the Oort Cloud. While the Oort Cloud has never beendirectly observed, its existence is firmly supported by the orbital characteristics oflong-period comets. Comets are icy dustballs, or dusty iceballs. They are compactaggregates of silicate dust and ices, within which organic compounds are trapped.Comets were formed at the outer reaches of the solar nebula, way beyond the“snowline” where water ice could condense.

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8.2Terrestrial Planets

8.2.1Mercury

Little is known about the planet Mercury: there are very few images of it, andbecause those that are available were taken during a flyby mission, namely, by theMariner 10 spacecraft in 1974, we have images of only one side of this planet (Fig.8.1). That situation will change in the coming decade, with both NASA’s MercurySurface, Space Environment, Geochemistry, and Ranging (MESSENGER) missionand ESA’s BepiColombo mission orbiting the planet Mercury. (BepiColombo isnamed after Professor Giuseppe (Bepi) Colombo (1920–1984), a mathematicianand engineer from the University of Padua, Italy. He was the first to see that anunsuspected resonance is responsible for Mercury’s habit of rotating on its axisthree times for every two revolutions it makes around the Sun. He also suggested toNASA how to use a gravity-assist swing-by of Venus to place the Mariner 10spacecraft in a solar orbit that would allow it to fly by Mercury three times in1974–1975). Mercury appears to be a highly cratered, gray, and lifeless body. It is aplanet of extremes, in temperature and radiation. The dayside of this heavilycratered planet is baked and cracked by the heat of the Sun, with temperaturesup to 450�C, while the night side is bitterly cold, with temperatures as low as–180�C. Its proximity to the Sun causes it to receive an incredibly high dose ofradiation, and its lack of a significant atmosphere ensures that the radiationpenetrates right down to the surface.The potential for Mercury to host life is very low but not completely negligible.

Although the temperature range experienced at its surface is extreme, there aresome regions where ice has been predicted, or observed, to occur. Radar images ofthe Polar Regions have been interpreted as showing the presence of water ice, andwhere there is ice there is the possibility of water and thus the possibility of life. Inaddition, the lack of tectonic activity on Mercury might allow organic molecules(delivered by comets and asteroids) to be preserved on the surface within the

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Fig. 8.1 South pole of Mercury, as photo-graphed by Mariner 10 in September 1974,showing bright craters that might containwater ice. The field of view is approximately1 000 km across, and was taken from a distanceof 85 800 km. (Image copyright: NASA/JPL/Northwestern University, Image No. PIA02941).

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regolith. It is known from observations of extremophile microorganisms on Earththat there are some microbes that thrive in high-radiation environments (seeChapter 5). Indeed, there are some microorganisms that survive inside nuclearplants, and so the surface radiation of Mercury might hold no fears for suchorganisms.

8.2.2Venus

Venus is Earth’s sister planet, the closest planet to us, and the two planets havemany similarities: size, composition, an atmosphere, and a similar gravity(Fig. 8.2). But in reality, Venus is very different from Earth. Venus can be summedup in three words: hot, smelly, and windy.

• Hot: the hottest surface in the Solar System, even hotter thanMercury, which lies much closer to the Sun. Temperatures atVenus’ surface are about 460 �C.

• Smelly: although Venus’ thick atmosphere, which is about 90times thicker than the terrestrial atmosphere, is mainly carbondioxide, it includes a very high percentage of sulfur dioxide.

• Windy: the thick atmosphere moves rapidly as the planetspins. The atmosphere is the key to why Venus is so hot – ittraps the Sun’s heat, so Venus is an extreme example of arunaway greenhouse.

Although the surface of Venus is unlikely to host life now, there has been spec-ulation by Schulze-Makuch and Irwin that life might have existed in the past, whenthe Sun was dimmer and cooler. The same authors have also speculated about thetype of organisms that might be able to exist in the lower cloud levels today (for acritical discussion, see Chapter 6). Results from ESA’s Venus Express mission,which arrived at Venus in April 2006, will yield more information about the planet.

8.2 Terrestrial Planets 207

Fig. 8.2 False color global mosaic from thesynthetic aperture radar instrument on theMagellan orbiter of the northern surface ofVenus. The north pole is at the center of theimage, with 0�, 90�, 180�, and 270� east longi-tudes at the 6, 3, 12, and 9 o’clock positions,respectively, of an imaginary clock face (ImageNo. PIA 00271, courtesy of NASA).

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8.2.3Earth

To date, Earth is the only planet within the Solar System that seems to have reachedits potential for hosting life. There is evidence of life all over the planet, in the mostextreme of environments. The time at which life arose on Earth is not known. Atsome point in its formation, between 4.57 and 3.5 billion years ago, Earth hadstabilized to the extent that there were three dynamically interacting reservoirs: theatmosphere, the lithosphere, and the hydrosphere. In addition, plate tectonics wastaking place, with a mechanism of plate movement close to that in operation today.The atmosphere was mildly reducing in composition and was composed of gasesincluding CO2 and CH4 (see Chapter 3 for more details).The presence of a biosphere at this early time is a matter of great debate: features

within sediments that were interpreted as fossilized microorganisms have recentlybeen reinterpreted as chemical traces, although there have been more recentreports of microbial biomarkers in 3.5-billion-year-old volcanic pillow laves (seealso Chapter 1). Over the next billion years, the composition of Earth’s atmospherechanged progressively. At around 2.3 billion years ago, the switch from a reducingto an oxidizing atmosphere became permanent, and the atmosphere had evolved toa composition closer to that observed today (see Chapter 6).The unambiguous establishment of life can be tracked through the fossil record,

with the first appearance of macrofossils about 600 million years ago. In the timeintervening between the emergence of life and the present day, microbes colonizedevery environment in which it is possible for life to survive. The conditionsprevailing in these “habitable niches” include extremes of temperature, salinity,and other extremes and are taken to define a “biological envelope” within which lifecan survive, grow, and evolve (see Chapter 5).

8.2.4Mars

Mars is one of the key planets with a high potential for life. Like Earth, Mars is arocky planet. It has a radius of approximately half and a mass around one-tenth thatof the Earth; consequently, gravity onMars is only about 40% of that on Earth. Mars’atmosphere is also different from that of the Earth: it is much thinner, around600 Pa (6 mbar), compared with 105 Pa (1 000 mbar), and consists of predominantlycarbon dioxide (about 95% CO2) rather than nitrogen (N2). The thin atmosphereprovides the Martian surface with little protection from heat loss; thus, the averagedaily temperature is around –60�C. Temperatures may reach +30�C at the equatorduring daytime in summer and fall to –130�C at the poles in winter.

8.2.4.1 Observing MarsThere have been many observations of Mars, by a variety of instruments andtechniques, and we are currently experiencing an unparalleled period of Martian

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exploration. One of the earliest scientific observers of Mars was Giovanni Schia-parelli. In 1882 he described canali, an Italian word meaning channels, and went onto give detailed descriptions of linear features on Mars’ surface. The most directtranslation of canali in English is canal, implicating that the features were artificial,i.e., had been made by Martians. An observer in America, Percival Lowell, spent agreat deal of his time at the beginning of the 20th century trying to show that therewas a very large network of interconnecting canals on Mars. The most recentobservations of Mars by telescope have been made by the Hubble Space Telescope(HST), which in 2001 produced detailed images showing the polar caps and themain features of the planet. When the HST image is matched to the mapsproduced by Schiaparelli in 1882 and Lowell in 1907, it becomes apparent thatthe earlier observers were, in fact, mapping areas of dust, not channels.It was not until the 1960 s that spacecraft visited Mars, enabling further

advances in understanding the features of the planet’s surface. Mariner 4, in1965, and Mariner 6 and Mariner 7, in 1969, were flyby missions that recordedimages of craters. Those missions also provided the first evidence that there wereno artificial canals on Mars. The first clear pictures of the Martian surface camefrom Mariner 9, a spacecraft that orbited the planet for almost a year from 1971 to1972. These first pictures of the surface of Mars from orbit showed in very greatdetail the channels and features that are now interpreted as river valleys. As ofApril 2006, there were four spacecraft in orbit around Mars: Mars Global SurveyorandMars Odyssey (both NASA missions) andMars Express (an ESA mission).MarsReconnaissance Orbiter, launched by NASA in August 2005, arrived in the vicinityof Mars in March 2006 and will commence science operations in November 2006.Orbiting the planet yields information on a global scale; more detailed localinformation is gained from landing craft on the surface and making measure-ments in situ.The first probes to land on Mars were Viking 1 and Viking 2 in 1976, followed by

Pathfinder in 1997. There are two landers that, at the time of this writing (May2006), are still in operation: NASA’s Mars Exploration Rovers (MERs) Spirit andOpportunity. The two rovers have been in operation for one Martian year, which isequivalent to about two terrestrial years (1 Martian year lasts 687 days). They havereturned detailed images and chemical analyses of the Martian surface. All of thelanding sites are within about 15 �N and 15 �S of the Martian equator, but across arange of longitudes.Much has been learned about Mars from telescope and spacecraft observations.

But there is an additional way of exploring Mars that employs the highly preciseinstrumentation of the laboratory-based astronomer. There is a group of 37meteorites that have come from Mars, and laboratory-based study by microscopeand other instruments has yielded information on the thermal, fluvial, and atmos-pheric history of the planet. One of the most important pieces of information thatcame from these studies is an absolute chronology for Martian specimens (seeSection 8.2.5).Given that Mars formed from the same starting materials as Earth, and that it

also suffered bombardment by comets delivering water and organic compounds

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throughout the Solar System, Mars is thought to have a high potential for support-ing life. In the following sections, evidence will be considered that the planet hasbeenmolded by fluvial and thermal processes, such that water and heat are, or havebeen, important in Mars’ history.

8.2.4.2 Evidence for WaterSince Mariner 4 in 1965, there have been more than 30 missions to Mars,experiencing greater or lesser success (see Chapter 13, Table 13.5). This fascinationwith Mars comes from its potential for hosting life that is based on abundantevidence of water on Mars. Ever since Schiaparelli observed his canali, we haveknown about channels onMars. Satellite images of the surface of Mars have shownmany features that have been interpreted as having been produced by water:images from all of the orbiting spacecraft from Mariner 9 onwards show networksof channels cutting the Martian surface. Some of the channels appear to be narrowand deep, while others are broader and flatter (Fig. 8.3). They show all the featuresexhibited by rivers on Earth at different ages. Older rivers on Earth meander acrossflat plains, producing features such as cutoff lakes and terraces; these too can beseen on images from Mars. Large-scale evidence for a frozen sea has also beenpublished, and it is thought that ice below the surface covered with dust created thefeatures (Fig. 8.4). Further indication of subsurface ice has come from results fromthe MARSIS radar instrument on Mars Express.The past five years have seen a dramatic increase in the number, resolution, and

quality of images and compositional data from Mars’ surface returned by bothorbiting satellites and rovers. One result of these data has been a gradual change inour perception of the fluvial history of Mars. The paradigm for many years was the“warmer and wetter” scenario, in which water was stable over vast areas of Mars’surface, implying a thicker atmosphere and warmer temperatures during pastepochs. It is now thought to be more likely that, apart from the very earliest period(the Noachian epoch, approximately the first 500million years), Mars has been cold

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Fig. 8.3 Martian river valley; part of the ReullVallis, east of the Hellas Basin (41 �S, 101�E)taken from a height of 273 km by the High-resolution Stereo Camera (HRSC) on MarsExpress. The area is 100 km across; north isat the top (Image credit: ESA/DLR/FU Berlin,G. Neukum).

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and dry for much of its history, with transient fluvial events, often short-livedcatastrophic flooding, triggered by increases in magmatic activity.Under a warmer-and-wetter regime, with pervasive and persistent bodies of

standing water, there would be an extended hydrological cycle in operation. Incontrast, a “cold and dry” climate for most of Mars’ history would curtail anyhydrological cycle. The difference between the two climate models is of greatsignificance for the potential evolution of life on Mars.Water alters the surface mineralogy of Mars: water-soluble salts are precipitated

as evaporites (typically minerals such as anhydrite, gypsum, and carbonates) andprimary silicate minerals are hydrated and altered to clay minerals and hydroxides.Such secondary alteration products have been identified by instruments onboardNASA’s Odyssey orbiter (the thermal emission spectrometer [THEMIS] and thegamma-ray spectrometer [GRS]) and onboard ESA’s Mars Express orbiter (theObservatoire pour la Mineralogie, l’Eau, les Glaces et l’Activit� [OMEGA] andthe Mars Express subsurface sounding radar altimeter [MARSIS]), as well as bydirect analysis of Martian rocks and soil. Data from the GRS onOdyssey have shownthat there are regions of Mars where H, assumed to be bound as water, is abundant.There is a high concentration of H at the poles from water ice in the polar caps. Butthere are also high concentrations of H around mid-latitudes and high northernlatitudes. Those concentrations are thought not to be from water as ice but insteadfrom water bound within minerals. This observation has been confirmed by datafrom the OMEGA instrument on the Mars Express orbiter, allowing the construc-tion of a relative chronology for the formation of secondary minerals from differentweathering regimes on Mars.Additional evidence for alteration of the surface by water has come from the

findings of NASA’s MERs Spirit and Opportunity. The rovers have been exploringtwo different parts of the surface of Mars for a Martian year. Spirit landed in GusevCrater, a shallow, flat-lying crater. As it explored the surface of the crater, it foundsharp angular fragments of rock littering the surface. Opportunity landed inMeridiani Planum, some thousands of kilometers to the east of Spirit’s landingsite. The panoramic camera aboardOpportunity acquired a panorama of the Paysonoutcrop on the western edge of Erebus Crater (Fig. 8.5). From the vicinity at thenorthern end of the outcrop, layered rocks are observed in the crater wall, which is

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Fig. 8.4 Martian sea; part of the ElysiumPlanitia near the Martian equator (5ºN; 150ºE)taken by the HRSC on Mars Express. The area isa few tens of kilometers across (Image credit:ESA/DLR/FU Berlin, G. Neukum).

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about 1 m thick. Some of those rocks had been disrupted by the crater-formingimpact event and subjected to erosion over time. Closer examination of those rockshas shown them to contain small spherules. These spherules weather out of therock and are present on the surface. It is thought that they were produced by theaction of water. They are weathering and evaporation products. The Mçssbauerspectrometer (see Chapter 12) on the rover Opportunity found the hydrated sulfatemineral jarosite present in the soil, showing that the rocks at Meridiani Planumhad been altered by water.

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Fig. 8.5 Panorama of the “Payson” outcrop on the westernedge of Erebus Crater acquired by the panoramic camera aboardNASA’s Mars Exploration Rover (MER) Opportunity (Imagecaption and credit: NASA/JPL–Caltech/USGS/Cornell).

Fig. 8.6 The complex caldera at the summit ofOlympus Mons (18.3 �N; 227�E) with a depth ofabout 3 km. The image was taken from a heightof 273 km by the HRSC on Mars Express. Theimage is about 100 km across; south is at thetop (Image credit: ESA/DLR/FU Berlin, G.Neukum).

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8.2.4.3 Evidence of HeatAs well as evidence of fluids on the surface of Mars, there is a great deal ofevidence from satellite imagery that Mars has had a significant thermal history.Mars has a core-mantle structure similar to that of Earth, but it seems to have arigid crust rather than the more flexible plate structure of the Earth, althoughrecent results from the magnetometer on NASA’s Mars Global Surveyor indicateevidence for limited tectonic spreading. This is shown by the presence, in theTharsis region in the western hemisphere of Mars, of a cluster of enormousvolcanoes, now presumably extinct. The largest of these volcanoes is OlympusMons, which is the biggest volcano in the Solar System. It is approximately threetimes higher than Mount Everest and the area of the volcano would cover that ofEngland plus Wales.The presence of these volcanoes indicates that an enormous amount of molten

rock or magma has erupted onto the Martian surface at times in the past. High-resolution images from the Mars Express camera show that Olympus Mons has acomplex crater, indicating that magma was erupted in several different episodes.As Fig. 8.6 shows, there are complex fault structures on the crater floor, formedfollowing eruption as the remaining rock in the underlying magma chambercooled and solidified. There are four other smaller craters within the large craterarea, indicating at least five periods of eruption.

8.2.5Meteorites from Mars

As detailed in Section 8.2.4, much about Mars can be learned through studying theplanet by telescope and spacecraft instrumentation. There is a third set of obser-vations of Mars, complementary to those made by remote means: data acquiredthrough laboratory analysis of Martian meteorites. Before detailing the under-standing we have gained about Mars from Martian meteorites, it will be explainedhow we know that the meteorites do indeed come from Mars.

8.2.5.1 Why from Mars?The meteorites in question were grouped together as the SNCs (after the typespecimens of the three original groups, Shergotty, Nakhla, and Chassigny). In thefollowing sections, these meteorites will be referred to as the SNCs until all theevidence surrounding their origins is detailed.The first clue that the SNCs were not conventional asteroidal meteorites came

from their age. The asteroids formed at the same time as the Solar System, some4 570 million years ago. The SNCs have much younger crystallization ages (asyoung as 165 million years old), implying that they cooled and solidified after thebulk of the Solar System formed. In other words, they came from bodies that werestill partially molten or still producing molten rock at least 165 million years ago. Inorder for molten rocks to exist on a body, the body must be very large, i.e., planet-sized. Thus, the SNCs come from a planet, not the asteroid belt. They do not

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originate from comets or Kuiper Belt Objects (including Pluto), which are assumednot to have melted.Therefore, the SNCmeteorites must have come from a planet, but which planet?

Although the giant planets have rocky cores, Jupiter and Saturn are mainly gas andUranus and Neptune are mixtures of gas and ice; the rocky cores are so deep belowthe thick atmospheres that it is unlikely that the meteorites came from the giantplanets. It is also unlikely that the meteorites came from the satellites of thoseplanets, because anything removed by impact would be captured by the giantplanets themselves. On the basis of dynamical impossibility, the planets Jupiter,Saturn, Uranus, and Neptune, and their satellites, are rejected as potential sourceobjects of these meteorites.Moving to the innermost part of the Solar System, Mercury is a rocky planet very

close to the Sun. It is very heavily cratered and thus it is clear that its surface isfrequently struck by asteroids; it is equally clear that material would be able toescape from Mercury’s small gravitational field. However, the proximity of Mer-cury to the Sun implies that much of the material leaving the Mercurian surfacewould be pulled straight into the Sun. There is, however, a small but finiteprobability that some material could leave Mercury and be ejected outwardsfrom the Sun towards the Earth. There was a suggestion that the unusual basalticmeteorite NWA 011 might be from Mercury, because this meteorite has an oxygenisotopic composition different from any other meteorite group, but the suggestionhas been neither verified nor taken seriously by meteoriticists.In contrast to Mercury, Venus is a large planet (about the size of Earth) and has a

very thick atmosphere (about 90 times thicker than Earth’s). It is energetically verydifficult to remove material from the Venusian surface by impact. For an asteroidto hit the surface of Venus, it must have sufficient energy to penetrate through thevery thick atmosphere without being fully ablated in order to leave sufficientmaterial available to create an impact crater on the surface. Following craterformation, impact ejecta would have to have sufficient energy to travel backthrough Venus’ thick atmosphere and still maintain sufficient energy to escapefrom Venus’ deep gravitational well. So, as in the case of Mercury, there is a smallbut finite chance of material being removed from Venus and impacting on theEarth. In fact, because Mercury is a small, atmosphere-less body, the probability ofremoving material from Mercury’s surface is greater than acquiring material fromVenus. Even so, it is not possible to discount Mercury and Venus as sources of theSNCs, although, as will be shown later, there is more compelling evidence thateliminates them as source objects.This logically leaves only three bodies as potential parents of the SNCmeteorites:

the Earth, its Moon, and Mars. First, we will consider the Earth–Moon system. TheMoon was long thought to be a possible source of meteorites. The Moon is crateredand, like Mercury, is a small and airless body. Objects that impact the Moon couldproduce craters from which material is readily ejected and, given the nearness ofEarth, fall on the Earth. But the Apollo and Luna samples returned directly from theMoon are so different in age and composition from the SNCs that the latter cannotbe from the Moon. However, lunar meteorites do exist, and the first one was

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recognized in 1983. The name of this meteorite is ALHA81005; it was collected inthe Allan Hills region of Antarctica in 1981. Analysis of ALHA81005 showed,without dispute, that the object came from the Moon. Its mineralogy, mineralchemistry, and isotopic composition, and the gases trapped inside it, were identicalto similar measurements made on the Apollo samples brought back from the Moonby astronauts in the 1970 s. There are now almost 50 lunar meteorites, and they arecompletely different from the SNCs. They are brecciated and rich in plagioclase,and all have ancient ages similar to the Apollo samples.If not from the Moon, could the meteorites have come from Earth? We know the

Earth is cratered, although many of the craters are hidden by vegetation or havebeen removed through plate tectonics and crustal recycling. It is easy to picture anasteroid impacting Earth’s surface and ejecting material. Perhaps this material didnot have quite sufficient energy to escape from Earth’s gravitational well and fellback to the surface, acquiring a fusion crust on the way and appearing as ameteorite. However, origin as a terrestrial rock can be eliminated on the groundsof the oxygen isotopic composition of the meteorites. Oxygen has three isotopes:16O (the major isotope), 17O, and 18O. On a three-isotope plot, all terrestrialmaterials that contain oxygen have an isotopic signature that falls on a specificline, the terrestrial fractionation line (TFL). As Fig. 8.7 shows, the TFL is welldefined, and the SNCs have oxygen signatures that do not fall on that line. Thisdoes not tell us where these meteorites came from, but it does tell us where they didnot come from.On the basis of oxygen isotopic composition, the SNCs did not come from Earth.

The pattern of variation in the oxygen isotopic signature of the rocks, however, issimilar to that of terrestrial rocks. In other words, they are spread out along astraight line that has a slope parallel to that of the TFL. This means that these rockscame from a single body, and that body is not Earth. It also is not the Moon, it isprobably not Mercury or Venus, and it is certainly not the asteroids, nor Pluto,Jupiter, Saturn, Uranus, or Neptune. That leaves only one body: Mars.On the basis of this negative deduction, the meteorites came from Mars.The specific observations that linked SNCmeteorites to Mars came with analysis

of gases trapped within one of the samples, the Antarctic meteorite namedElephant Moraine (EET) A79001. This meteorite contains inclusions of black glassscattered throughout its mass. The glass was formed by shock melting of mineral

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Fig. 8.7 Oxygen isotopic composition ofSNC meteorites (filled symbols) compared withthe TFL. The data appear to fall along a singlefractionation line parallel to the TFL; this line islabeled as the Martian Fractionation Line (afterFranchi et al. 1999).

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grains, presumably during the impact event that lofted the meteorite from thesurface of its parent body. Analysis of gas trapped within the glass during theimpact shock showed that it was identical in composition to that of the atmosphereon Mars, as measured by the Viking landers in 1976 (Fig. 8.8). The only way thatthis could happen is if EET A79001 came from Mars. Based on their oxygenisotopic composition, all the other SNC meteorites came from the same parentas EET A79001; therefore, they too must have come from Mars.

8.2.5.2 What can we Learn About Mars from Martian Meteorites?The 37 different Martian meteorites are subdivided into four main groups. Collec-tion of additional Martian meteorites from Antarctica and the Sahara Desert hasextended the number of subgroups to five. The subgroups are rocks that formed indifferent locations at or below the Martian surface. The groups have differentmineralogies and chemistries and cannot all have come from a single impact event.At least three craters, with minimum diameters of about 12 km, are required toproduce the variety of Martian meteorite types. Measurements made on Martianmeteorites complement data obtained from spacecraft exploration of Mars, anduntil we have a mission that returns material directly from Mars, these meteoritesare the only objects that we have to help us understandMartian geology, in additionto in situ investigations by Martian rovers.The largest of these groups of Martian meteorites is the shergottites, after the

type specimen Shergotty, which is subdivided into three subgroups.

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Fig. 8.8 Comparison of the composition of Mars’ atmospherewith gas trapped in the shergottite EETA79001 (after Pepin 1985).

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The basaltic shergottites are fine-grained cumulate rocks composed of almostequal amounts of clinopyroxene and plagioclase. The plagioclase has been con-verted, by shock, to maskelynite glass. Alignment of the minerals indicates that therocks originated in a lava flow.The lherzolitic shergottites are also cumulates but are more coarse-grained than

the basaltic shergottites, indicating a slower cooling rate; they formed deeper belowthe Martian crust than the basaltic shergottites, and their terrestrial equivalentwould be a peridotite. The main silicate is orthopyroxene, enclosing olivine grains,with minor plagioclase.The olivine-phyric shergottites are composed of large olivine and orthopyroxene

grains set in a finer-grained clinopyroxene matrix. They are thought to be fromolivine-saturated magmas that were parental to those from which basaltic shergot-tites crystallized.All three subgroups of shergottites have crystallization ages of 165–450 million

years. However, it has been discussed that this age in fact could be an alteration agecaused by reaction of surface fluids with the rocks. This is still a topic for discussionand research. At least two cratering events ejected shergottites fromMars into space;these events happened in much more recent times, 0.5–3 million years ago.The second main group of Martian meteorites is that of the nakhlites, named for

their type specimen Nakhla. Their dominant minerals are the silicates augite andolivine, which are altered to clay minerals along cracks and fractures. The nakhlitesare almost unshocked rocks that formed at or near the Martian surface in a thickflow. They solidified from melts about 1.3 billion years ago and were ejected fromthe planet about 10–12 million years ago. The meteorites have been altered byweathering on Mars’ surface, leading to the production of secondary minerals, e.g.,clays, carbonates, and sulfates, which are associated with low concentrations ofMartian organic material. It has thus been suggested that nakhlites might containevidence for a Martian biosphere.The recognition of complex assemblages of salt (halite) with carbonates and clay

minerals in nakhlites has allowed interpretation of the scale and mode of fluid flowon the surface of Mars. Results from the nakhlites imply that when water waspresent on the surface, it was warm and briny and restricted in flow. In otherwords, it might have been locked in enclosed basins that occasionally overflowed inepisodes of flash flooding.The third group of Martian meteorites is the chassignites, named for the type

specimen Chassigny. The mineralogy of the chassignites is different from that ofthe nakhlites and the shergottites. They are highly shocked olivine cumulates; ifthey were terrestrial rocks, they would be described as dunites. Like the nakhlites,the chassignites have a crystallization age of 1.3 billion years, implying somerelationship between the two groups.The final subset of Martian meteorites is composed of a single member, Allan

Hills 84001. This unusual meteorite is predominately composed of orthopyroxene.It is riddled throughout with millimeter-sized patches of rimmed carbonates,showing that although this is an igneous rock, like the nakhlites, it too has sufferedaqueous alteration. It is the oldest of all the Martian meteorites, having crystallized

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about 4.5 billion years ago, and has had a long and complex history of shock andthermal metamorphism. Because few hydrated minerals – such as those found inclays on Earth – have been identified among the alteration products in ALH84001,it has been proposed that the carbonates were produced at the surface of Mars in aregion of restricted water flow, such as an evaporating pool of brine.The seven groups of Martian meteorites are all igneous rocks, and from them we

can learn about processes on Mars. There are three types of information we cangain from these rocks. The first is information about primary magmatism onMars:the meteorites are igneous rocks, and they have crystallized from the flows ofMartian volcanoes or within subsurface magma chambers. Therefore, studying thecomposition andmineralogy of these rocks helps us to understand the temperatureand mode of volcanism on Mars.The secondary alteration products in thesemeteorites help us to learn about fluid

flow on the surface of Mars. Particularly in ALH84001 and in the nakhlites, thecomplex assemblages of secondary minerals shed light on the temperature andsalinity of the water that flowed across Mars’ surface. The zoned nature of some ofthe minerals tells us how fluid composition has changed, either in terms oftemperature or in terms of the salts dissolved in the fluid. The restricted natureof some of these alteration assemblages also indicates the restricted nature of thatfluid flow (perhaps fluid that was combined to an evaporating basin rather than to ariver or a stream).The third type of information that we can gain from Martian meteorites is

associated with shock. The shergottites and the chassignites are shocked meteor-ites, and they contain patches of the glass maskelynite formed by the conversion ofplagioclase during shock melting and quenching. Trapped within these meltpockets is Mars’ atmosphere; as outlined above, this was the clue that finallyconfirmed the Martian origin of these rocks. By looking at Martian meteorites ofdifferent ages and at the gas trapped in the rocks of different ages, it is possible thatwe might be looking at samples of Mars’ atmosphere trapped at different times. Itis also possible that we might be able to trace the evolution of Mars’ atmosphere bylooking at these pockets of gas.

8.2.5.3 Microfossils in a Martian Meteorite?The observation that at least one of the SNCs, EETA79001 (a specimen found in theElephant Moraine region of Antarctica in 1979), contained indigenous, i.e., Mar-tian, organic material associated with carbonate minerals sparked a debate on thepossibility of Martian meteorites containing evidence for extraterrestrial life. In1994 this work was followed by the discovery of similarly enhanced levels of organiccarbon in close association with carbonates in a second Antarctic Martian meteor-ite, ALH84001.ALH84001 became a further focus of interest in 1996 when a team of scientists

led by David McKay of NASA’s Johnson Space Center in Houston reported thedescription of nanometer-sized features within carbonate patches in ALH84001and claimed to have found evidence of primitive “fossilized Martian biota.” Iden-

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tification of the features as nanofossils remains controversial because much of theevidence is circumstantial and relies on the coincidence between a number ofotherwise unrelated characteristics of the meteorite, particularly the association oforganic materials with carbonates. One specific aspect of the claim was that withinthe carbonates were tiny grains of magnetite, which seemed to form chains. Thosechains of grains were interpreted as being reminiscent of traces from magneto-tactic bacteria. However, other scientists have argued that these grains of magnetiteare natural products within the meteorite and are not connected at all with any typeof bacterium. Indeed, the formation conditions of both the carbonate and magnet-ite, the relevance of the organic compounds, and the interpretation of the mor-phology of the “nanofossils” have all been subject to detailed investigation byseveral groups of scientists.More recently, the same team investigated carbonaceous features in Nakhla that

they have posited might have a biological origin. Although many members of thescientific community are skeptical about interpretation of the structures inALH84001 and Nakhla, discussion of the features has stimulated an enormousamount of interest in the possibilities of life on Mars.

8.2.6Can We Detect Signatures of Life on Mars?

Whether or not the features in the Martian meteorites are remnant fossilizedMartian bacteria, the debate has highlighted one of the difficulties of searchingfor fossil microorganisms on any planet, including Earth. The most ancient fossillife on Earth was, until recently, thought to be microfossils of the Apex chert inwestern Australia. However, recent work has reinterpreted these structures as non-biological. The point I am trying to make here is that on Earth one can return to thelocality from which the microfossils were collected and obtain fresh material; onecan study them in situ and in the context of the rocks and geology around them.One can use every technique available to analyze these features, but still one cannotsay for certain whether they are biological or not. Thus, relying on the morphology,the appearance only, of microfossils, whether on Earth or on Mars, is not going todeliver the definitive answer of how to detect life.So how should and how could one detect life on Mars? There was an instrument

on the recent unfortunate Beagle 2 lander (see Chapter 12) that would haveperformed the type of experiment that would help us understand whether lifewas present onMars. The Gas Analyze Package (GAP) was a mass spectrometer onthe Beagle 2 lander; it was constructed to determine the isotopic composition ofcarbon in Mars’s soil. The experiment would have taken a small chip of rock andheated it up slowly in the presence of oxygen (O); O would burn carbon (C). Thetemperature at which C burns gives information on the type of component present,whether it is a simple organic molecule or is more complex, whether it is acarbonate or is carbon trapped or dissolved in primary magmatic minerals. Bylooking at the speciation of C and its isotopic composition, GAP would have madethe measurements that would allow us to build up a C cycle for Mars. We would

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have been able to put limits on the different reservoirs on Mars’ surface and assesswhether or not there was evidence for life on Mars.One of the next chances for detecting signatures of life on Mars will be with the

European mission ExoMars, to be launched in 2013 (see Chapter 12). The ExoMarsrover will carry a comprehensive suite of analytical instruments, including thePasteur payload, dedicated to searching for signs of past and present life on Mars,especially in subsurface samples, by a suite of coordinated investigations.

8.2.7Conclusions: Life Beyond Earth?

To summarize, we have not yet found life (extant, dormant, or extinct) on Mars, orany evidence that it arose on Mars. There are several missions planned to Mars inthe coming decade, but we do not know whether any one of them will be successfulin finding life on Mars. Looking at the astrobiology of the terrestrial planets, it hasbeen shown that Mars is indeed, at least within the rocky inner planets, the bestplace other than Earth to look for life.Other targets to be considered in astrobiology are the non-terrestrial planets, or,

more specifically, their satellites. Titan, the biggest moon of Saturn, has beendescribed as a laboratory for prebiotic Earth, and results from the recent Huygensprobe have confirmed that interesting chemistry is certainly occurring there (seeChapter 9). Results from the Cassini mission have indicated that Enceladus seemsto have water, and Europa, one of Jupiter’s Galilean satellites, was identified asprobably possessing a subsurface ocean (see Chapter 10). The possibilities of lifebeyond Mars are discussed in other chapters within this book.

8.3Further Reading

8.3.1Concerning Planetary Formation and Chronology

Halliday, A. N., Kleine, T. Meteorites and thetiming, mechanisms, and conditions of ter-restrial planet accretion and early differen-tiation, in: D. Lauretta (Ed.) Meteorites andthe Early Solar System II, Univ. ArizonaPress, 775–801, 2006.

Lissauer, J. J. Planet formation, Ann. Rev. As-tron. Astrophys. 1993, 31, 129–174.

Wadhwa, M., Russell, S. S. Timescales of ac-cretion and differentiation in the early SolarSystem: the meteoritic evidence, in: A. Boss,V. Manning, S. Russell (Eds.) Protostars andPlanets IV,University of Arizona Press, 995–1018, 2000.

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8.3.2Concerning Recent Results from Mars

Bibring, J.-P., Langevin, Y., Gendrin, A., Gon-det, B., Poulet, F., Berth�, M., Soufflot, A.,Arvidson, R., Mangold, N., Mustard, J.,Drossart, P. Mars surface diversity as re-vealed by the OMEGA/Mars Express obser-vations, Science 2005, 307, 1576–1581.

Christensen, P. R., Wyatt, M. B., Glotch, T. D.,Rogers, A. D., Anwar, S., Arvidson, R. E.,Bandfield, J. L., Blaney, D. L., Budney, C.,Calvin, W.M., Fallacaro, A., Fergason, R. L.,Gorelick, N., Graff, T. G., Hamilton, V. E.,Hayes, A. G., Johnson, J. R., Knudson, A. T.,McSween, H. Y., Mehall, G. L., Mehall, L. K.,Moersch, J. E., Morris, R. V., Smith, M. D.,Squyres, S.W., Ruff, S.W., Wolff, M. J.Mineralogy at Meridiani Planum from theMini-TES Experiment on the OpportunityRover, Science 2004, 306, 1733–1739.

Klingelhçfer, G., Morris, R. V., Bernhardt, B.,Schrçder, C., Rodionov, D. S., de Souza,

P. A., Yen, A., Gellert, R., Evlanov, E. N.,Zubkov, B., Foh, J., Bonnes, U., Kankeleit,E., G�tlich, P., Ming, D.W., Renz, F., Wdo-wiak, T., Squyres, S.W., Arvidson, R. E.Jarosite and Hematite at Meridiani Planumfrom Opportunity’s Mçssbauer Spectrome-ter, Science 2004, 306, 1740–1745.

Squyres, S.W., Grotzinger, J. P., Arvidson,R. E., Bell, J. F., Calvin, W., Christensen,P. R., Clark, B. C., Crisp, J. A., Farrand,W.H., Herkenhoff, K. E., Johnson, J. R.,Klingelhçfer, G., Knoll, A. H., McLennan,S.M., McSween, H. Y., Morris, R. V., Rice,J. W., Rieder, R., Soderblom, L. A. In situevidence for an ancient aqueous environ-ment at Meridiani Planum, Mars, Science2004, 306, 1709–1714.

Tokano, T. (Ed.) Water on Mars and Life,Springer Berlin Heidelberg New York, 2005.

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8.3.3Concerning Terrestrial and Martian Microfossils

Brasier, M. D., Green, O. R., Jephcoat, A. P.,Kleppe, A. K., Van Kranendonk, M. J., Lind-say, J. F., Steele, A., Grassineau, N. V.Questioning the evidence for Earth’s oldestfossils, Nature 2002, 416, 76–81.

McKay, D. S., Gibson, E. K., Thomas-Keprta,K. L., Vali, H., Romanek, C. S., Clemett, S. J.,Chiller, X. D. F., Maechling, C. R., Zare,

R. N. Search for past life on Mars: Possiblerelic biogenic activity in Martian meteoriteALH84001, Science 1996, 273, 924–930.

Schopf, J.W., Kudryavtsev, A. B., Agresti,D. G., Wdowiak, T. J., Czaja, A. D. Laser-Raman imagery of Earth’s earliest fossils,Nature 2002, 416, 73–76.

8.3.4Concerning Meteorites from Mars

Bogard, D. D., Johnson, P. Martian gases inan Antarctic meteorite? Science 1983, 221,651–654.

Bridges, J. C., Catling, D. C., Saxton, J. M.,Swindle, T. D., Lyon, I. C., Grady M.M. Al-teration assemblages in Martian meteorites:implications for near-surface processes,Space Sci. Rev. 2001, 96, 365–392.

Franchi, I. A., Wright, I. P., Sexton, A. S., Pil-linger, C. T. The oxygen-isotopic composi-tion of Earth and Mars, Meteorit. Planet. Sci.1999, 34, 657–661.

McSween, H. Y., Jr. What we have learnedaboutMars from SNCmeteorites,Meteoritics1994, 29, 757–779.

Nyquist, L. E., Bogard, D. D., Shih, C.-Y., Gre-shake, A., Stçffler, D., Eugster, O. Ages andgeologic histories of Martian meteorites,Space Sci. Rev. 2001, 96, 105–164.

Pepin, R. O. Evidence of Martian origins, Na-ture 1985, 317, 473–475.

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8.4Questions for Students

Question 8.1Outline the main reasons that the meteorite EET A79001 is believed to come

from Mars.Question 8.2Why is Mars thought to be a possible place to search for life?Question 8.3What can we learn about Mars from Martian meteorites?

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9Astrobiology of Saturn’s Moon TitanFranÅois Raulin

The chapter presents the astrobiological case for Titan, the largestsatellite of Saturn. Besides Jupiter’s moon Europa, Titan appears tobe the most interesting body for astrobiology in the outer SolarSystem because it has an active prebiotic-like chemistry, but liquidwater is absent on its surface. This chapter starts with a descriptionof the general properties of Titan and models of its formation andinternal structure. Emphasis is placed on the astrobiological as-pects, which are based on spacecraft observations, above all therecent Cassini–Huygens mission, on laboratory experiments sim-ulating the atmospheric conditions of Titan, and on photochemicalmodeling. On the basis of those data, current astrobiological as-pects of Titan are considered with regard to analogies with the earlyEarth, extraterrestrial organic (even prebiotic-like) chemistry, andpossibilities for life.

9.1Extraterrestrial Bodies of Astrobiological Interest

The following are different types of extraterrestrial bodies of prime interest forastrobiology:

• planetary bodies where life may be present, either extinct orextant,

• other bodies where a complex organic chemistry is takingplace, and

• bodies that may show some similarities with our own planetEarth, particularly the early Earth, before the emergence oflife.

The best examples of the first category are our neighbor planet Mars (see Chapter8) and Europa, one of the Galilean satellites of Jupiter, because of its potential foran internal water ocean (see Chapter 10). In fact, with the exception of Io, the

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majority of the Galilean satellites seem to have a water ocean in their internalstructure (Fig. 9.1) and thus are of interest for astrobiology. Recent data, providedby the infrared (IR) spectrometer of the Cassini–Huygens mission, identifiedSaturn’s moon Enceladus as a body of high astrobiological interest. The temper-ature at its south pole is very high, comparable to that of the Earth, and may allowthe presence of liquid water on its surface.Comets and carbonaceousmeteorites are the best example of the second category

(see Chapter 3). Titan, the largest satellite of Saturn and the only satellite in theSolar System having a dense atmosphere (Fig. 9.2), combines all three aspects.

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Fig. 9.1 Possible internal structure of the four Galilean satellites(adapted from NASA/JPL).

Fig. 9.2 Mosaic of Titan’s surface from imagestaken by the narrow-angle camera of the Cassinispacecraft. The large bright-white area is calledXanadu. The resolution is about 1.3 km perpixel (image credit: NASA/JPL/Space ScienceInstitute).

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Therefore, Titan is considered one of the most interesting bodies of the SolarSystem with regard to astrobiology.Many data have been obtained and are still expected from the Cassini–Huygens

mission, a cooperative project of the U. S. National Aeronautics and Space Admin-istration (NASA), the European Space Agency (ESA), and the Italian Space Agency(ASI). Future astrobiological exploration missions to Titan are under considera-tion. With an active organic chemistry, but in the absence of permanent liquidwater on the surface, Titan already looks like another world: a natural laboratory forprebiotic-like chemistry.

9.2Some Historical Milestones in the Exploration of Titan

On 25 March 1655, the Dutch astronomer Christiaan Huygens (1629–1695), withhis newly constructed 2-inch diameter lens of 12-foot focal length (providing a 50magnification), was observing Saturn and detected an enigmatic prominent object,three minutes of arc away from the giant planet. By continuing the observation overseveral nights, he noted that this object was following Saturn’s trajectory. He thusdeduced that it was amoon of Saturn. He was even able to calculate that this satelliteorbits its planet within 16 terrestrial days. Much later, in 1847, this largest moon ofSaturn was named “Titan” by John Herschel (1792–1871). According to the Romanmythology, Titan is one of the siblings of Saturn, the god of agriculture.While observing Titan in 1908, the Spanish astronomer Jos� Comas-Sola (1868–

1937) reported seeing limb darkening around the disk of the satellite. Thisobservation suggested the presence of an appreciable atmosphere around Titan.However, this report was received with skepticism within the scientific commun-ity, because Comas-Sola had reported similar observations for most of the Galileansatellites. Finally, his conclusion was taken seriously into consideration by theBritish astronomer James Jeans (1877–1946).Jeans, author of the theory of thermal atmospheric escape, carried out a math-

ematical study of the possible escape of an atmosphere from planetary bodies. Hedetermined that a body like Titan can keep a substantial part of its atmosphere,despite its relatively small size (with a diameter on the order of 5 000 km), if thetemperatures of its environment are low enough (ranging from about 60 K to100 K). More precisely, the escape rates for all species with a molecular massexceeding about 16 Da will be very small at those low temperatures.In the winter of 1943–1944, the American-Dutch astronomerGerard Pieter Kuiper

(1905–1973) observed Titan from the 82-inch McDonald Observatory (Mount Locke,Texas) using photographic emulsions sensitive up to the near infrared (0.7 �m). Heobtained a spectrum showing the absorption bands of gaseous methane (CH4). Thiswas the confirmation that Titan indeed has an atmosphere, and it demonstrated thatthis atmosphere includesmethane as one of its constituents. Kuiper was even able tocalculate the abundance of methane and derived from his observations that thepartial pressure of methane at Titan’s surface should be about 0.1 bar (100 hPa).

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The presence of methane in the gaseous phase was confirmed later on by manyobservations from ground-based telescopes, before the Titan flyby maneuvers ofNASA’s Pioneer 11 spacecraft in 1979 and of Voyager 1 in 1980, one of NASA’s twinVoyager spacecraft.

9.3General Properties, Formation and Internal Structure of Titan

9.3.1Main Properties

In Table 9.1 the main general properties of Titan are listed. With a radius R of2 575 km, Titan is the largest satellite of Saturn and is the second largest satellite ofthe Solar System, after Ganymede (R = 2 631 km), one of the Galilean Jovianmoons. But if one takes into account its dense atmosphere and extends its radiusup to the stratopause, Titan reaches a radius of 2 875 km, which makes it thelargest moon in the Solar System. Like Saturn, Titan’s mean distance from the Sunis about 9.5 astronomical units (AU) and its period of rotation around the Sun – asgiven by Kepler’s third law (see Chapter 7) – is about 30 years. The solar flux at thelocation of Titan is about 1% of the flux at the level of Earth orbit (remember thatthe radiation decreases with the square of its distance from the source). The meantemperature of Titan, if considered as a black body, is about 82 K.

Table 9.1 Main characteristics of Titan (including HASIHuygens data).

Property Value

Surface radius 2 575 kmSurface gravity 1.35 m s–2 (0.14 Earth’s value)Mean volumic mass 1.88 kg dm–3 (0.34 Earth’s value)Distance from Saturn 20 Saturn radii (~1.2 � 106 km)Orbit period around Saturn ~16 daysOrbit period around Sun ~30 years

Atmospheric data

Altitude (km) Temperature (K) Pressure (hPa)Surface 0 93.7 1 470Tropopause 42 70.4 135Stratopause ~250 ~187 ~1.5 � 10–1

Mesopause ~490 ~152 ~2 � 10–3

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Titan is in fact the only satellite of the Solar System that has a noticeableatmosphere. Its atmosphere is made mainly of nitrogen, with a substantial per-centage of methane. The surface pressure is 1.5 bar (1 500 hPa) and the surfacetemperature is about 94 K. This temperature is higher than the black body temper-ature because of a noticeable greenhouse effect of about 20 K caused by some of theatmospheric constituents (mainly methane and dihydrogen) and despite an anti-greenhouse effect of about 8 K produced by the haze particles. The consequence ofthese temperature and pressure (T, P) conditions is that Titan’s atmosphere nearthe surface is about five times denser than the Earth’s atmosphere.The inclination of Titan on its orbit around Saturn is small (0.33 �). Because

Titan’s equatorial plane is practically in Saturn’s ring plane, Titan has seasons likeSaturn, which has an obliquity of 27�. A complete rotation of Titan around Saturntakes 16 days, with synchronous rotation. But while the solid surface of Titanrotates slowly, the satellite exhibits a super-rotation of its atmosphere due to strongzonal winds (similar to the case of Venus, with its very dense atmosphere; seeChapter 8). Titan’s orbit is slightly eccentric (e = 0.029): this provides some con-straints on its internal structure and suggests the absence of a shallow ocean on itssurface (which would tend to reduce the eccentricity value and change the orbittoward a circular one). Its distance from Saturn is about 20 Saturnian radii, farenough to avoid interactions with the Saturn rings and still small enough to allowTitan’s atmosphere to interact regularly with the electrons of Saturn’s magneto-sphere.Another detail of paramount importance to astrobiology is the mean density of

the satellite, which is 1.88 g cm–3. This value is equivalent to that of Ganymede(about 1.9 g cm–3) and much smaller than that of Jupiter’s satellite Europa (about3 g cm–3). The low density of Titan indicates an internal structure made of low-density materials such as water (in solid and possibly liquid phase) and, moregenerally, ices of a mean density of approximately 1 g cm–3, mixed with high-density materials such as rocks and silicates with a mean density of about 3 g cm–3.This information is important when modeling the formation of the satellite.

9.3.2Models of Formation and Internal Structure

Like the other satellites of Saturn, Titan originated about 4.6 billion years ago fromSaturn’s subnebula. Titan grew up out of the accretion of small blocks andplanetesimals present in the subnebula; during that process, the temperatureincrease generated mainly by gravity processes and radioactive decay was able tomelt the icy components, and the rocks sunk toward the center of the planetarybody. The resulting body was probably made of an undifferentiated inner silicatecore, mixing rocks and ices, covered by a silicate outer core and a liquid mantle of awater–ammonia mixture, and dominated by a dense atmosphere. The origin andcomposition of this primordial atmosphere is still under debate. One classicalscenario, developed by Prinn and Fegley in 1981, assumes that the early subnebulaof Saturn was convective and stable and that carbon was mainly in the form of

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carbon monoxide (CO) and nitrogen in the form of N2. At the location of Titan’sorbit, which is 20 Saturn radii, the temperature and pressure conditions were highenough to allow the conversion of CO into CH4 and N2 into ammonia (NH3). ThenCH4 and NH3 would have been trapped in the form of hydrates in the planet-esimals forming Titan. The specificity of Titan, compared to all of Saturn’s othersatellites, can consequently be explained by the particular position of its site offormation within Saturn’s subnebula, as recently published by Sekine and cow-orkers (2005).A different scenario, developed by Mousis et al. (2002), supposes that the

subnebula of Saturn was turbulent and that CO and N2 could not be efficientlyconverted into CH4 and NH3 under such conditions. The subnebula thus containedCO and some CH4 and N2 and some NH3. Models of the evolution of suchsubnebula show that in the feeding zone of Saturn, were the planetesimals areformed, CH4 and NH3 were efficiently trapped as hydrates, contrary to CO and N2.The relics of such CH4/NH3-rich planetesimals were thus used to form Titan. Inthis case, the composition of the atmosphere should reflect the volatile componentsof those planetesimals.Both models assume that CH4 and NH3 were progressively released in the

atmosphere and that NH3 was converted into N2 by photochemical processes inthe upper regions of the atmosphere or even by impact shock–catalyzed dissocia-tions. From such models of Titan’s formation, it is possible to derive the resultinginternal structure of Titan after 4.6 billion years of evolution.After a relatively short period (about 100 million years) of a warm aqueous

environment induced by efficient energy sources, those energies became lessabundant and Titan’s surface cooled down. Water started freezing out of the

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Fig. 9.3 Internal structure of Titan. (a) primordial Titan;(b) present Titan (adapted from Fortes 2000).

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H2O–NH3 solution, thereby forming an ice I crust. (Ice I is the form of all naturalsnow and ice on Earth.) Its thickness rapidly increased, reaching 30 km in (only)70 million years. The high pressure at the bottom of the ocean induced thecrystallization of water ice VI and ammonia hydrates. (Ice VI is formed fromliquid water at 1.1 GPa by lowering its temperature to 270 K.) This process shouldhave enriched Titan’s ocean in ammonia. The depth and composition of theresulting ocean depended on the heat flow from the core and its convectivetransport to the surface. Recent models by Tobie and coworkers (2005) indicatethat the ocean might have contained up to 15 wt% of NH3 over a depth of about200 km (Fig. 9.3).

9.4Atmosphere and Surface of Titan

As in many scientific fields, one can consider three main and complementaryapproaches to studying a planetary body.

• One approach is theoretical modeling, e.g., with regard tophotochemistry, thermodynamics, and microphysics. In thecase of planetary astrobiology, it allows one to follow theevolution of organics within time durations that are un-reachable experimentally and to provide estimates of theirconcentrations in different space locations.

• The second approach is experimental, involving laboratorysimulations with specific experiments. With these ad hoctools, by developing experiments in the laboratory, one canobtain detailed information about the studied object (of as-trobiological interest).

• The last approach is observation, which includes remotesensing from Earth and spacecraft and in situmeasurements.This is an essential and perfect approach to constrain themodels, both theoretical and experimental, and to provide, bycoupling the observational data with the other information,an integrated comprehensive vision of the studied body.

9.4.1Theoretical Modeling of Titan’s Atmosphere

In a high-temperature system, one can derive the composition of the main and tracespecies by assuming thermodynamic equilibrium and calculating the distribution ofspecies from their standard free energies of formation. The result of such calcu-lation, based on relatively simple chemical equilibrium calculation, has the advant-age of being independent of the reactions that have been considered. However, inthe case of a low-temperature system, such as Titan’s atmosphere, the equilibriumstate is not reached. Therefore, this approach is more than questionable.

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In the case of low-temperature systems, kinetic modeling is a safer method. It ispossible to determine the steady-state composition that can be reached in any partof the system by the following approach. First, all chemical reactions involved inthe system need to be identified, and their corresponding rate constants at the righttemperatures must be obtained. Further, the spatial distribution of energy includ-ing the radiative transfer aspects must be known, as well as the diffusion constantsfor both molecular and eddy diffusions. From a set of chosen chemical reactions(which can be numerous!), a differential equation between concentration, time,and space coordinates (altitude z in a 1D model) can be written for each compoundin a given location of the system. With adequate software these equations cansimultaneously be solved. Thus, a steady state can be written for each constituent i(Eq. 1)), where ni is the concentration of the constituent, Pi its production rate, Li itsloss rate, �i its vertical flux, Ci its condensation factor, and z the altitude. Theresolution of these equations gives the concentration of i as a function of the spacecoordinate (altitude z in a 1D model).

dni=dt ¼ Pi � niLi � dçi=dz� Ci (9.1)

Several kinetic models, mainly photochemical models, of Titan’s atmosphere havealready been published. Until now, the data (mainly the vertical concentrationprofiles) derived from these models were relatively poorly constrained by observa-tional data, because only a few observations provided reliable concentration valuesat a given altitude. Furthermore, the models involved eddy diffusion coefficient, theprofile of which is poorly known.Nevertheless, these models provide a quite good understanding of the chemical

processes involved in this complex atmospheric chemistry. The primary processesinvolve the dissociation of CH4 and N2 by the solar UV photons and the electrons

9 Astrobiology of Saturn’s Moon Titan230

Fig. 9.4 Chemical and physicalprocesses in Titan’s atmosphereaccording to chemical modeling.

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from Saturn’s magnetosphere. The resulting primary species formed in the highatmosphere yield to the production of simple hydrocarbons and N-compounds,especially C2H2 and HCN (Fig. 9.4). These two molecules play a key role in thegeneral chemical scheme. Once they are formed, they diffuse down to the loweratmospheric regions, where the available UV photons are less energetic but areabsorbed by the two compounds, which leads to their dissociation (Fig. 9.5). Theresulting radicals allow the formation of more-complex hydrocarbons and nitriles.In the chemical processes, polyynes, such as C4H2 and C6H2, and cyanopolyynes,such as HC5N, may play an important role in the formation of high-molecular-weight products. Additional CH4 dissociation probably occurs in the low strato-sphere through photocatalytic processes involving C2H2 and polyynes. The endproduct of this chemistry would be a macromolecular organic compound mademainly of C, H, and N.If a species is omitted in a theoretical model, this will not change the results of

thermodynamic equilibrium calculations. On the contrary, kinetic prediction maystrongly depend on the nature of the assumed mechanism, and the omission of animportant reaction may render the result invalid. Furthermore, contrary to ther-modynamic data, many of the data feeding the photochemical models are notavailable. This is the case, for instance, with kinetic constants, especially at lowtemperatures and for complex species, as well as with UV and IR spectra andquantum yields and branching ratios of photodissociation reactions. The simplecase of methane photodissociation with Lyman alpha photons (121.6 nm) clearlyillustrates the problem. As shown in Table 9.2, the values of quantum yields and ofbranching ratios are quite variable from one author to another. This may inducestrong uncertainties in the photochemical model, which then propagate.

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Fig. 9.5 Energy depositionin Titan’s atmosphere.

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Table 9.2 Quantum yield of the primary process of photo-dissociation of methane by Lyman alpha radiation (121.6 nm)obtained by different models.

Reaction Quantum yield

Model A[a] Model B[a] Model C[b] Model D[c]

CH4 + h� � CH3 + H 0.51 0.49 0.41 0.291CH4 + h� � CH2 + H + H 0.25 0 0 0.055CH4 + h� � CH2 + H2 0.24 0 0.53 0.584CH4 + h� � CH + H + H2 0 0.51 0.06 0.07

Source: Adapted from H�rbrard (2006).a Model by Mordaunt and coworkers (1993).b Model by Smith and Raulin (1999).c Model by Wang and coworkers (2006).

A new model is currently being developed by this author’s group to study theinfluence of these uncertainties in the model inputs on the output data of themodel. This new 1-D model includes 121 neutral species, 20 photodissociations

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Fig. 9.6 1-D photochemical modeling of Titan: vertical distributionof HC3N and associated uncertainties derived from the uncertain-ties in rate constants and photolysis rates. Several available ob-servational data are plotted for comparison (from H�brard 2006).

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with 50 branches, and 664 chemical reactions with associated reaction rates. It uses260 atmospheric layers and implies the resolution of 31 460 nonlinear, highlycoupled equations. The propagation of chemical uncertainties in the model in-duces strong uncertainties in the vertical concentration profiles, as shown inFig. 9.6 for HC3N. These uncertainties have strong consequences on the conclu-sions that can be inferred from the models. With the resulting error bars, themodeled vertical profile fits with most of the observations, suggesting that it isdifficult to constrain the chemical scheme of the model without having a betterprecision of the input parameters. In any case, the information provided by suchwork can be used for identifying the reactions for which kinetic data and otherassociated parameters are essential and need to be experimentally determined.

9.4.2Experimental Approach

Different types of laboratory experiments related to the study of planetary environ-ments can be considered. In particular, experiments are specifically designed fordetermining some of the parameters involved in the evolution of the planetarybody, such as rate constant or thermodynamic equilibrium data or spectroscopicdata (IR, UV, radio-wave, and so forth). Other experiments are developed tosimulate partly or globally the evolution of the considered environment. Such so-called “simulation experiments” can integrate the many different physical andchemical processes involved. One of the first simulation experiments carried out inthe laboratory is the classic Stanley Miller experiment, which is supposed to mimicthe chemical evolution processes in the conditions of the primitive Earth environ-ment (see Chapter 3). In the absence of any direct observational data of such anenvironment, this was indeed a unique tool. More recently, several groups haveused a similar approach to study the evolution and organic chemistry of Titan’satmosphere.This type of experiment requires a reactor with the following specifications:

• a judiciously chosen energy source that adequately mimicsthe sources really present in the atmosphere and that is ableto break the chemical bonds of the molecules constituting theinitial gas mixture representing the main composition ofTitan’s atmosphere;

• a good vacuum device to prepare and introduce this initial gasmixture into the reactor and to sample the resulting products;and

• efficient analytical tools for analyzing the products, in boththe gas and condensed phases.

Through sampling and chemical analysis, the evolution of the system then can befollowed and the results extrapolated to the real case. In fact, the design anddevelopment of the experiment is not so simple, and it requires careful preparationand great care. The right choice of the numerous parameters involved is essential,

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e.g., the abundance of the constituents in the starting gas mixture, the pressure, theenergy flux, the temperature, etc.Further, the design of the reactor, the nature of the energy source, and the

analytical procedures are essential. The reaction vessel may induce some wall effect,which is of course absent in the atmosphere of Titan and whichmay bias the results.Simulating processes in the high atmosphere, where pressure is low and three-bodycollisions are not favored, requires the use of large reactors. Under such conditions,the products may be very diluted and difficult to analyze. On the other hand, whenusing small, closed reactors, the accumulation of products makes their analysiseasier, but it may significantly alter the primary processes compared to the planetaryconditions. Indeed, within such conditions, the composition of the gas mixturechanges and no longer represents the main composition of the simulated atmos-phere. This issuemay be avoided by using a flow reactor, which is usually coupled toan electron impact energy source, such as a cold plasma discharge.In Titan’s atmosphere the main energy sources are solar UV radiation and mid-

energy electrons coming fromSaturn’smagnetosphere (Fig. 9.5). OnlyUVphotons ofwavelengths shorter than about 150 nm can dissociate methane. The most abundantsolar photons in this range of wavelengths are Lyman alpha (121.6 nm) photons. Thisradiation can easily be simulated in the laboratory by using monochromatic lamps.But the Lyman Æ line does not allow the photodissociation of N2, which requiresphotons of a wavelength shorter than about 100 nm. UV radiation of such shortwavelengths is difficult to obtain in the laboratory with irradiation systems compatiblewith closed reactors or even with flow reactors. For this reason, all laboratory experi-ments simulating the chemical evolution of Titan’s atmosphere that have been carriedout so far on N2–CH4 initial gas mixtures use an electron impact energy source thatmimics Titan’s atmospheric electrons impinging from Saturn magnetosphere. An-other approach compatible with a short-wavelength UV source is the use of an initialgasmixture with another N-compound that can be photodissociated byUV photons oflonger wavelengths and is also present in Titan’s atmosphere – although at tracelevels. Examples include the molecules HCN and HC3N.Since the flyby of Titan by the two Voyager spacecrafts in the early 1980 s (which

provided a first determination of the main properties of its atmosphere, includingits main composition and vertical temperature and pressure structure), manyexperiments have been carried out to simulate Titan’s atmospheric chemistry inthe laboratory.In the gas phase, more than 150 different organic molecules have been detected

in simulation experiments.These global simulations of Titan’s atmospheric chemistry use an open reactor

with a continuous flow of a low-pressure N2–CH4 gas mixture (Fig. 9.7). The energysource is a cold plasma discharge producingmid-energy electrons (around 1–10 eV).The gas-phase end products (molecules) are analyzed by infrared Fourier transformspectroscopy (IRFTS) and gas chromatography and mass spectrometry (GC-MS)techniques. The transient species, i.e., radicals and ions, are determined by onlineultraviolet-visible (UV–VIS) spectroscopy. The evolution of the system is theoret-ically described using coupled physical and chemical models.

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The identified organic products are mainly hydrocarbons and nitriles. Theabsence – at a detectable level – of molecules carrying amino groups, such asamines, with the exception of ammonia, must be highlighted. In these experi-ments all gaseous organic species observed in Titan’s atmosphere were detected.Among the organics that were formed in simulation experiments, but that are not(yet) detected in Titan’s atmosphere, one should note the presence of polyynes suchas C4H2, C6H2, C8H2, and probably cyanopolyyne HC4-CN. These compounds arealso included in photochemical models of Titan’s atmosphere, where they mightplay a key role in the chemical schemes allowing the transition from gas-phaseproducts to aerosols. Of further astrobiological interest is the formation of organiccompounds with asymmetric carbon.Recent experiments by Bernard and coworkers on N2–CH4 mixtures including

CO at the 100-ppm level show the incorporation of oxygen (O) atoms in theproduced organics, with an increasing diversity of the products. More than 200different compounds were identified. The main O-containing organic compoundfound is oxirane – also called ethylene oxide – (CH2)2O. Oxirane thus appears to bea good candidate to search for in Titan’s atmosphere.Further, simulation experiments produce solid organics, usually called tholins, a

generic name invented by Carl Sagan in the late 1970 s. These “Titan tholins” aresupposed to be laboratory analogues of Titan’s aerosols. They have been extensivelystudied since the first work by Sagan and Khare more than 20 years ago. Theselaboratory analogues show very different properties depending on the experimentalconditions. For instance, in the many published reports, the average C:N ratio ofthe product may vary between values of less than 1 and more than 11.Recently, dedicated experimental protocols allowing a simulation closer to real

conditions have been developed in this author’s laboratory using low pressure andlow temperature and recovering the laboratory tholins without oxygen contamination(from the air of the laboratory) in a glove box purged with pure N2. Representativelaboratory analogues of Titan’s aerosols thus have been obtained and their complexrefractive indices determined, for the first timewith error bars. These data represent anew point of reference for modelers who are computing the properties of Titan’saerosols. Systematic studies have been carried out on the influence of the pressure ofthe starting gas mixture on the elemental composition of the tholins. They show that

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Fig. 9.7 Experimental setup for global simula-tion of Titan’s atmospheric chemistry at LISA(Laboratoire Interuniversitaire des Syst�mesAtmosph�riques, Universit�s Paris 12 et Paris 7).A gas mixture of N2 (98%) and CH4 (2%) flowscontinuously through the open reactor and ismaintained at low pressure (~1 hPa) and lowtemperature (~150 K) (image credit: P. Coll).

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two different chemical-physical regimes are involved in the processes, depending onthe pressure, with a transition pressure around 1 hPa.The molecular composition of the Titan tholins is still poorly known. Several

possibilities have been considered, including HCN polymers or oligomers, HCN-C2H2 co-oligomers, HC3N polymers, and HC3N-HCN co-oligomers. It is wellestablished that they are made of macromolecules of largely irregular structure.Gel filtration chromatography of the water-soluble fraction of Titan tholins showsan average molecular mass of about 500–1000 Da. Information on the chemicalgroups included in their structure has been obtained from their IR and UV spectraand from analysis by pyrolysis GC-MS techniques. The data show the presence ofaliphatic and benzenic hydrocarbon groups, of CN, NH2, and C=NH groups. Directanalysis by chemical derivatization techniques before and after hydrolysis allowedthe identification of amino acids and their precursors. Their optical properties havebeen determined because of their importance for retrieving observational datafrom Titan. Finally, it obviously is of astrobiological interest to mention that thenutritious properties of Titan tholins for terrestrial microorganisms have also beenstudied, showing that some microorganisms can indeed use them as nutrients.There is still a need for more-accurate experimental simulations, where the

primary processes are well mimicked, including the dissociation of N2 by electronimpact with energies close to those of Titan’s atmosphere and the dissociation ofmethane through photolysis processes. Such an experiment is currently underdevelopment at this author’s laboratory, which is called SETUP (SimulationExp�rimentale et Th�orique Utile � la Plan�tologie).

9.4.3Observational Approach

Of course, neither of the two previous approaches can be developed without anyobservational data. As mentioned above, much information on Titan has beenobtained from ground-based observations, before and even after Voyager’s flyby ofTitan in 1980 and 1981. Several instruments of the Voyager spacecraft providedfurther insight into Titan’s atmosphere. For example, the determination of theatmospheric composition was obtained from observations by the infrared interfer-ometer spectrometer and radiometer (IRIS) – in the IR range – and the ultravioletspectrometer (UVS) – in the UV range. The vertical atmospheric structure from200 km altitude to the surface was derived from the data of the radio-occultationexperiment. Later observations from ground-based and Earth-orbiting space tele-scopes, such as NASA’s Hubble Space Telescope (HST) and ESA’s Infrared SpaceObservatory (ISO) provided additional data on Titan’s atmospheric composition andeven – for the first time – Titan’s surface heterogeneities, by using dedicatedspectral windows and adapted optics.The NASA-ESA Cassini–Huygens mission is an excellent example of an observa-

tional approach to study Titan, because it combines both remote sensing and in situobservations. The Cassini–Huygens spacecraft was successfully launched from CapeCanaveral, Florida, USA, on 15 October 1997 by use of a Titan IVB/Centaur rocket.

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The spacecraft – which consisted of a Saturn orbiter, the Cassini spacecraft, and aTitan atmospheric probe, the Huygens entry probe – was on a seven-year interplan-etary trajectory toward Saturn that relied on four gravity-assist maneuvers at Venus(1998 and 1999), Earth (August 1999), and Jupiter (December 2000) to reach its finaldestination (Fig. 9.8; see Chapter 7 for more information on gravity-assist maneu-vers). It reached Saturn in 2004, with a Saturn orbit insertion on 1 July 2004. Sincethat date, Saturn has a new – but artificial – satellite, the spacecraft Cassini. Cassiniembarked on a four-year tour of the Saturnian system, whichmay last longer with anextended mission. At the end of 2004, after two initial Titan encounters, it releasedtheHuygens probe on the third orbit around Saturn on 25 December 2004.Huygenspenetrated Titan’s atmosphere and parachuted down to the surface on 14 January2005. The descent lasted about 2.5 hours, and Huygens continued functioning forthree hours on the surface. Cassini recovered surface data for more than 1 hour and10 minutes, before it went out of the field of view of the landed probe.The Cassini–Huygens mission was designed to explore the Saturnian system in

great detail, including the giant planet, its atmosphere, its magnetosphere andrings, and many of its moons, especially Titan, by using the 12 scientific instru-ments onboard the spacecraft (Table 9.3). Titan’s exploration is one of the mainobjectives of the mission, which includes multiple opportunities for close remotesensing and observations of Titan by the Cassini orbiter. During the four years of

9.4 Atmosphere and Surface of Titan 237

Fig. 9.8 Interplanetary trajectory of the Cassini spacecraft. Afterthe insertion in the Saturn orbit on 1 July 2004, Cassini released theHuygens probe on 25 December 2004. The probe penetratedTitan’s atmosphere on 14 January 2005 (image credit: NASA/JPL).

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the nominal mission (mid-2004 to mid-2008), the planned 74 orbits around Saturninclude 44 close Titan flybys.

Table 9.3 Instruments on the Cassini spacecraft, interdiscipli-nary programs (IDP), the leading scientists, and the potential forastrobiological return of their investigation.

Instrument or IDP PI, team leader,or IDS[a]

Country Astrobiologicalreturn

Optical remote sensing instrumentsComposite infrared spectrometer (CIRS) V. Kunde, M. Flasar USA +++Imaging science subsystem (ISS) C. Porco USA +++Ultraviolet imaging spectrograph (UVIS) L. Esposito USA ++VIS/IR mapping spectrometer (VIMS) R. Brown USA ++

Fields, particles, and waves instrumentsCassini plasma spectrometer D. Young USA +Cosmic dust analysis E. Gr�n Germany +Ion and neutral mass spectrometer H. Waite USA +++Magnetometer D. Southwood, M. Dougherty UK Not applicableMagnetospheric imaging instrument S. Krimigis USA Not applicableRadio and plasma wavespectrometer

D. Gurnett USA Not applicable

Microwave remote sensingCassini radar C. Elachi USA +++Radio science subsystem A. Kliore USA ++

Interdisciplinary programMagnetosphere and plasma M. Blanc France +Rings and dust J.N. Cuzzi USA +Magnetosphere and plasma T.I. Gombosi USA +Atmospheres T. Owen USA +++Satellites and asteroids L.A. Soderblom USA +Aeronomy and solar wind interaction D.F. Strobel USA ++

a PI: principal investigator, IDS: interdisciplinary scientist.

Several instruments of the orbiter and most of the six instruments of the probe(Table 9.4) provide data of astrobiological interest (Fig. 9.9). The optical remotesensing instruments of the orbiter, especially the composite infrared spectrometer(CIRS), the ion and neutral mass spectrometer (INMS), and the ultraviolet imagingspectrograph (UVIS), determine the chemical composition of different zones ofTitan’s atmosphere. They are able, in particular, to detect many organics, includingnew species, and allow the determination of their vertical concentration profile.The cameras of the imaging science subsystem (ISS), the Cassini radar, and thevisual and IR mapping spectrometer (VIMS) map Titan’s surface through the hazelayers and determine the morphology, the heterogeneity, the presence of craters,

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which may result from volcanic activity and from impactors, and information onthe chemical composition of the surface.

Table 9.4 Instruments on the Huygens entry probe,interdisciplinary programs (IDP), the leading scientists, andthe potential for astrobiological return of their investigation.

Instrument or IDP PI or IDS[a] Country Astrobiologicalreturn

Gas chromatograph-massspectrometer (GC-MS)

H. Niemann USA +++

Aerosol collector and pyrolyzer G. Isra�l France +++Huygens atmospheric structureinstrument

M. Fulchignoni Italy ++

Descent imager/spectralradiometer (DISR)

M. Tomasko USA +++

Doppler wind experiment M. Bird Germany +Surface science package (SSP) J. Zarnecki UK +++Interdisciplinary programAeronomy D. Gautier France ++Atmosphere/surface interactions J.I. Lunine USA ++Chemistry and exobiology F. Raulin France +++

a PI : principal investigator, IDS : interdisciplinary scientist

9.4 Atmosphere and Surface of Titan 239

Fig. 9.9 Images of Titan taken from the Cassinispacecraft. (a) False-color composite image ofTitan taken by the ISS wide-angle camera(combining near-IR and visible images) in April2005 at about 170 000 km distance. Resolutionin the images is approximately 10 km per pixel;

(b) Ultraviolet image of Titan’s night-side limb,taken by the narrow-angle camera. It showsmany fine haze layers extending several hun-dred km above the surface (image credit:NASA/JPL/Space Science Institute).

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The GC-MS instrument on the Huygens probe, a gas chromatograph (GC) withthree GC capillary columns coupled to a quadrupole mass spectrometer (MS),performed a detailed chemical analysis of the atmosphere – including molecularand isotopic analysis – during the 2.5 hours of descent of the probe. After landing,it continued with measurements of the surface. The aerosol collector and pyrolyzer(ACP) experiment collected atmospheric aerosols and heated them up to hightemperatures, which pyrolyzed the refractory part of the collected particles. Thenthe produced gases were transferred to the GC-MS instrument for molecularanalysis. This was the first direct in situmolecular and elemental analysis of Titan’shazes. The Huygens atmospheric structure instrument (HASI) determined, inparticular, the vertical profiles of pressure and temperature. The descent imager/spectral radiometer (DISR) measured the radiation budget of the atmosphere,investigated the cloud structure, and took images of the surface (Fig. 9.10A). Thesurface science package (SSP) provided information on the physical state andchemical composition of the surface.A paramount scientific synergy is given by the complementarities of the Cassini

observations, which on the one hand provide a global mapping of Titan by theCassini spacecraft with observations of potential temporal and spatial variationsand on the other hand provide very detailed information of one particular locationof Titan from the data of the Huygens entry probe.

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Fig. 9.10 Surface features of Titan and theEarth. (A) Channel networks, highlands, anddark-bright interface on the surface of Titanas seen by the DISR instrument on Huygens at

6.5-km altitude (image credit: ESA/NASA/JPL/University of Arizona); (B) A similar dentriticstructure seen on the Earth in the Yemendesert (image credit: NASA).

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9.5Astrobiological Aspects of Titan

9.5.1Analogies with Planet Earth

Titan’s dense atmosphere, which extents up to about 1500 km, is composedmainlyof N2, like the atmosphere of the Earth. The other main constituents are CH4,which amounts to about 1.6–2% in the stratosphere as measured by the CIRS onCassini and the GC-MS on Huygens, and H2, which amounts to about 0.1%.Despite the differences between Titan and the Earth, in particular in temperatureranges, there are several analogies between both bodies, as outlined below.The first resemblances concern the vertical atmospheric structure (see Fig. 9.5).

Although Titan is much colder, with a troposphere (~94 to ~70 K), a tropopause(70.4 K), and a stratosphere (~70–175 K), its atmosphere presents a similar com-plex structure and includes, like the Earth, as recently evidenced by Cassini-Huygens, a mesosphere and a thermosphere. With a much higher density in thecase of Titan, the mesosphere extends to altitudes higher than 400 km (instead ofonly 100 km for the Earth), but the shape looks very much the same.These analogies are linked to the presence of greenhouse gases and anti-green-

house elements in both atmospheres. CH4 has strong absorption bands in themedium- and far-IR regions, which corresponds to the maximum of the IRemission spectrum of Titan. CH4 is transparent in the near-UV and visible (VIS)spectral regions. It thus can be a very efficient greenhouse gas in Titan’s atmos-phere.H2, which absorbs in the far IR (through bimolecular interaction of its dimers),

plays a similar role. In the pressure–temperature conditions of Titan’s atmosphere,CH4 can condense but H2 cannot. Thus, on Titan CH4 and H2 are equivalent toterrestrial condensable H2O and non-condensable CO2. In addition, the hazeparticles and clouds in Titan’s atmosphere have an anti-greenhouse effect similarto that of the terrestrial atmospheric aerosols and clouds.Methane on Titan seems to play the role of water on Earth, with a complex cycle

that still is not well understood. Although the possibility that Titan is covered withhydrocarbons oceans has been ruled out, it is now likely that Titan’s surfaceincludes small lakes of methane and ethane, which seem to have been observedby the Cassini radar. The ISS camera on Cassini has also detected dark surfacefeatures near Titan’s south pole that might be such liquid bodies (see Fig. 9.14).Moreover, the DISR instrument on Huygens has provided pictures of Titan’ssurface, which clearly show dentritic structures (Fig. 9.10A) that look like aterrestrial fluvial net (Fig. 9.10B). Because these features are free of crater impacts,it is suggested that they lie in a relatively young terrain and that in this area liquidwas flowing recently on the surface of Titan. In addition, the Huygens GC-MS datashow that the CH4 mole fraction increases in the low troposphere (up to 5%) andreaches the saturation level at an altitude of approximately 8 km, allowing thepossible formation of clouds and rain. Furthermore, GC-MS observed an increase

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of about 50% in the CH4 mole fraction at Titan’s surface, suggesting the presenceof condensed methane at the surface in the vicinity of the Huygens probe.Other observations from the Cassini instruments clearly show the presence of

various surface features of different origin that are indicative of volcanic, tectonic,sedimentological, and meteorological processes, similar to those that are found onEarth (Fig. 9.10). One can push the analogies between Titan and the Earth evenfurther by comparing Titan’s winter polar atmosphere and the terrestrial Antarcticozone hole, although they imply different chemistries.INMS on Cassini and GC-MS on Huygens have detected the presence of argon

(Ar) in Titan’s atmosphere. As in the Earth’s atmosphere, the most abundantisotope is 40Ar, which comes from the radioactive decay of 40K. Its stratosphericmole fraction is about 3 � 10–5 as measured by GC-MS. The abundance of primor-dial argon (36Ar) is about 200 times smaller. The other primordial noble gases haveamixing ratio of less than 10 ppb. This strongly suggests that Titan’s atmosphere isa secondary atmosphere, produced by the degassing of trapped gases. Because N2

cannot be efficiently trapped in the icy planetesimals that accreted and formedTitan – in contrast to NH3 – this high abundance of N2 indicates that Titan’sprimordial atmosphere was initially made of NH3. Ammonia was then trans-formed into N2 by photolysis and/or impact-driven chemical processes. The14N:15N ratio measured in the atmosphere by INMS and GC-MS was 183 in thestratosphere, which is 1.5 times less than that of the primordial nitrogen. This lowratio indicates that the atmosphere was probably lost several times during thehistory of the satellite. Such evolution may also lead to methane transformationinto organics (see Section 9.5.2), which may suggest large deposits of organics onTitan’s surface.Lastly, analogies can be drawn between the organic chemistry that is now very

active on Titan and the prebiotic chemistry that proceeded in the environment ofthe primitive Earth (see Chapter 3). Despite the absence of permanent bodies ofliquid water on Titan’s surface, several of the organic processes that occur today onTitan imply the existence of some of the organic compounds considered to be keymolecules in terrestrial prebiotic chemistry. Examples include hydrogen cyanide(HCN), cyanoacetylene (HC3N), and cyanogen (C2N2). Indeed, a complex organicchemistry seems to be present in the three components of what one can call – byanalogy with our planet – the “geofluids” of Titan: air (gas atmosphere), aerosols(solid atmosphere), and surface (oceans).

9.5.2Organic Chemistry

Several organic compounds have already been detected in Titan’s stratosphere(Table 9.5). The list includes hydrocarbons (with both saturated and unsaturatedchains) and nitrogen-containing organic compounds, which are exclusively ni-triles, as expected from laboratory simulation experiments. Most of these detec-tions were performed by Voyager observations, with the exceptions of C2 hydro-carbons, which were observed before; acetonitrile, which was detected by ground

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observation in the millimeter wavelength; and water and benzene, which weretentatively detected by the ISO spacecraft. Since Cassini’s arrival in the Saturnsystem, the presence of water and benzene has been unambiguously confirmed bythe CIRS instrument. In addition, the direct analysis of the ionosphere by theINMS instrument during Cassini’s flybys of Titan shows the presence of manyorganic species at detectable levels (Fig. 9.11), despite the spacecraft’s high altitudeof 1 100–1 300 km.

Table 9.5 Main composition and detected trace components ofTitan’s stratosphere and comparison with products of laboratorysimulation experiments.

Compound Stratosphericmixing ratio

Location Simulationexperiments[a]

Main constituentsNitrogen N2 0.98Methane CH4 0.02Hydrogen H2 0.0006–0.0014

HydrocarbonsEthane C2H6 1.3 � 10–5 Equator Major productAcetylene C2H2 2.2 � 10–6 Equator Major productPropane C3H8 7.0 � 10–7 Equator ++Ethylene C2H4 9.0 � 10–8 Equator ++Propyne C3H4 1.7 � 10–8 North pole +Diacetylene C4H2 2.2 � 10–8 North pole +Benzene C6H6 Few 10–9 +

N-organicsHydrogen cyanide HCN 6.0 � 10–7 North pole Major productCyanoacetylene HC3N 7.0 � 10–8 North pole ++Cyanogen C2N2 4.5 � 10–9 North pole +Acetonitrile CH3CN Few 10–9 ++Dicyanoacetylene C4N2 Solid phase North pole +

O-compoundsCarbon monoxide CO 2.0 � 10–5

Carbon dioxide CO2 1.4 � 10–8 EquatorWater H2O Few 10–9

a ++: abundance smaller by one order of magnitude than that of the major product;+: abundance smaller by two orders of magnitude than that of the major product.

Surprisingly, the GC-MS instrument onboard theHuygens probe has not detected alarge variety of organic compounds in the low atmosphere. The mass spectracollected during the descent show that the medium and low stratosphere andthe troposphere are poor in volatile organic species, with the exception of CH4. Thismay be explained by the condensation of those high-molecular species on aerosol

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particles. These particles, for which no direct data on the chemical compositionwere available before, have been analyzed by the ACP instrument. ACP wasdesigned to collect aerosols during the descent of the Huygens probe on a filterin two different regions of the atmosphere. Then the filter was heated in a closedoven at different temperatures and the produced gases were analyzed by GC-MS.The results showed that the aerosol particles are made of refractory organics thatrelease HCN and NH3 during pyrolysis. This result strongly supports the tholinshypothesis (see Section 9.4.2). Based on these new and, for the first time, in situdata, it seems very likely that the aerosol particles are made of a refractory organicnucleus, covered with condensed volatile compounds (Fig. 9.12). The nature of thepyrolysates provides information on the molecular structure of the refractorycomplex organics. It indicates the potential presence of nitrile groups (-CN), aminogroups (-NH2, -NH- and -N<), and /or imino groups (-C=N-).Furthermore, comparison of the data obtained from the first sampling, which

consisted mainly of stratospheric particles, and the second one, which was taken inthe mid-troposphere, indicates that the aerosol composition is homogeneous. Thisfits with some of the data obtained by DISR on aerosol particles, which indicate arelatively constant size distribution of the particles with altitude. Their meandiameter is on the order of 1 �m.

9 Astrobiology of Saturn’s Moon Titan244

Fig. 9.11 Mass spectrum of Titan’sionosphere near 1200 km altitude. Thespectrum shows signatures of organiccompounds including those with up to7 carbon atoms (image credit: NASA/JPL/University of Michigan).

Fig. 9.12 Model of the chemical composition of Titan’s aerosolsderived from the Huygens ACP data.

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These particles sediment to the surface, where they form a deposit of complexrefractory organics and frozen volatiles. DISR collected the infrared reflectancespectra of the surface with the help of a lamp that illuminated the surface beforetheHuygens probe touched down. The retrieving of these infrared data showed thepresence of water ice but no clear evidence – so far – of tholins. The presence ofwater ice is supported by the data from SSP. Its accelerometer measurements canbe interpreted by the presence of small water ice pebbles on the surface whereHuygens has landed, in agreement with the DISR surface pictures (Fig. 9.13). Onthe other hand, GC-MS was able to analyze the atmosphere near the surface formore than one hour after touchdown. The corresponding mass spectra showed theclear signature of many organics, including cyanogen, C3, and C4 hydrocarbonsand benzene, indicating that the surface is much richer in volatile organics thanthe low stratosphere and the troposphere. These observations are in agreementwith the hypothesis that in the low atmosphere of Titan most of the organiccompounds are in the condensed phase.Altogether, these new data of the Cassini–Huygens mission show the diversity of

the locations where organic chemistry is taking place on Titan. Surprisingly, thehigh atmosphere looks very active, with neutral and ion organic processes; the highstratosphere, where many organic compounds had already been detected beforeCassini arrived in the Saturn system, shows an active organic chemistry in the gasphase. In the lower atmosphere, this chemistry seems to be concentrated mainly inthe condensed phase. Titan’s surface is probably covered with frozen volatileorganics together with refractory, tholin-like organic materials.Cosmic rays reaching Titan’s surface and hence these compounds may induce

additional organic syntheses, especially if part of these materials is dissolved in

9.5 Astrobiological Aspects of Titan 245

Fig. 9.13 Surface of Titan as seen by the DISR cameraon Huygens after it landed (image credit: ESA/NASA/JPL/University of Arizona).

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some small liquid bodies made of low-molecular-weight hydrocarbons (mainlymethane and ethane).Despite the low surface temperatures, the presence of liquid water is not

excluded. Cometary impacts on Titan may melt surface water ice, offering possibleepisodes of liquid water as long as about 1 000 years, as suggested by Artemievaand Lunine (2003). This scenario provides conditions for short periods of terres-trial-like prebiotic syntheses at relatively low temperatures. Low temperaturesreduce the rate constants of prebiotic chemical reactions but may increase theconcentration of reacting organics by an eutectic effect, which increases the rate ofthe reaction. In addition, the possible presence of a water–ammonia ocean in thedepths of Titan, as expected from models of its internal structure, may provide anefficient way to convert simple organics into complex molecules and to reprocesschondritic organic matter into prebiotic compounds. These processes may havevery efficiently occurred at the beginning of Titan’s history – with even thepossibility of the water–ammonia ocean exposed to the surface – allowing aCHON (carbon, hydrogen, oxygen, and nitrogen) prebiotic chemistry evolving tocompounds that may be of astrobiological interest.

9.5.3Life on Titan?

In the following sections, conditions are considered that may drive the chemistry inTitan’s environment from organic chemistry to prebiotic chemistry or maybe evento biotic processes. The overarching question is whether Titan’s conditions arecompatible with those needed for sustaining life (see also Chapter 6). The surfaceof Titan is too cold and not energetic enough to provide the right conditions forhabitability. However, the (hypothetical) subsurface oceans on Titan may besuitable for life, as suggested by Fortes (2000). The temperature of these hypo-thetical subsurface oceans is estimated as high as about 260 K. In addition,cryovolcanic hotspots are assumed with possible temperatures in the range of300 K. These temperature conditions might allow the development of livingsystems. Even at a depth of 200 km, the expected pressure of about 500 MPa(5 kbar) is not incompatible with life, as shown by terrestrial examples. Theexpected pH of an aqueous medium made of 15% by weight of NH3 is equivalentto a pH of 11.5. Some bacteria can grow on Earth at pH 12 (see Chapter 5). Even thelimited energy resources do not exclude the sustaining of life.Taking into account the potential radiogenic heat flow (about 5 � 1011 W) and

assuming that 1% of this is used for volcanic activity and 10% of the latter isavailable for living system metabolism, Fortes (2000) has estimated an energy fluxof about 5 � 108 W that may be available in Titan’s subsurface oceans. Consideringthe terrestrial biosphere, such a flux corresponds to the production of about4 � 1011 mol of ATP per year and about 2 � 1013 g of biomass per year. Assumingan average turnover for the living systems on the order of one year, the biomassdensity would be 1 g m–2. This number is very small compared to the lower limit ofthe value of the biomass for the Earth, which amounts to about 1000–10 000 g m–2.

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Nevertheless, these energetic considerations would allow a possible presence oflimited, but not negligible, bioactivity on the satellite. Assuming that extraterres-trial living systems are similar to the ones we know on Earth, and based on thechemistry of carbon and the use of liquid water as solvent (see Chapter 6), thehypothetical biota on Titan, if any, might be localized in the subsurface deep ocean.Several possible metabolic processes have been postulated for the hypotheticalsubsurface oceanic life on Titan, such as nitrate/nitrite reduction or nitrate/dinitrogen reduction, sulfate reduction or methanogenesis (Simakov 2001), andcatalytic hydrogenation of acetylene (Abbas and Schulze-Makuch 2002).As expected, no sign of macroscopic life has been detected by theHuygens probe

when approaching the surface or after landing. This can be concluded in particularfrom the many pictures taken by the DISR of the same location on Titan duringmore than one hour after landing. But this does not exclude the possibility of thepresence of microscopic life. The metabolic activity of a corresponding biota, evenif it is localized far from the surface in the deep internal structure of Titan, mayproduce chemical species that diffuse through the ice mantle, covering the hypo-thetical internal ocean, and feed the atmosphere. It has even been speculated inseveral publications that the methane seen in the atmosphere today is the productof biological activity. If this were the case, the atmospheric methane would benotably enriched in light carbon. On Earth, biological processes induce an isotopicfragmentation that produces enrichment in 12C. The ratio 12C:13C increases from89, which is the reference value taken from the Belemnite of the Pee DeeFormation, to about 91–94 depending on the biosynthesis processes. The 12C:13Cratio of atmospheric methane on Titan is 82, as determined by the GC-MS instru-ment on Huygens. Although we do not have a reference value for 12C:13C on Titan,this low value suggests that the origin of methane is likely to be abiotic.

9.6Outlook: Astrobiology and Future Exploration of Titan

Although exotic life such as methanogenic life in liquid methane cannot be fullyruled out, the presence of extant or extinct life on Titan seems very unlikely.Nevertheless, with the new observational data provided by the Cassini–Huygensmission, the largest satellite of Saturn appears more than ever to be an interestingobject for astrobiology. The several similarities of this exotic and cold planetarybody with the Earth (see Section 9.5.1) and the complex organic chemical processesthat are going on now on Titan (see Section 9.5.2) provide a fantastic means for abetter understanding of the prebiotic processes, which are no longer reachable onthe Earth at the scale and within the whole complexity of a planetary environment.The origin and cycle of methane on Titan illustrate the whole complexity of the

Titan system. Methane may be stored in large amounts in the interior of thesatellite as clathrates (methane hydrates) trapped during the formation of thesatellite from the Saturnian subnebula, where it was formed by Fischer-Tropschprocesses (abiotic synthesis of hydrocarbons from CO and H2 using metallic

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catalysts). It may also be produced through high-pressure processes, such asserpentinization, allowing the formation of H2 by reaction of H2O with ultramaficrocks, or by cometary impact. Interestingly, these processes have rarely beenconsidered in the case of the primitive Earth, although they may have contributedto a possible reducing character of the primordial atmosphere of the Earth. Thatpossibility was recently reexamined by Tian and coworkers (2005). This is anexample of how the study of Titan is indeed bringing some new ideas to theunderstanding of chemical evolution processes on the early Earth.In Titan’s atmosphere, methane is photolyzed by solar UV radiation, whereby

mainly ethane and tholin-like organic matter are produced. The resulting lifetimeof methane in Titan’s atmosphere is relatively short (about 10–30 million years).Thus, methane stored in Titan’s interior may be continuously replenishing theatmosphere by degassing induced by cryovolcanism, which has been clearlyevidenced by the first images of Titan’s surface provided by the VIMS, ISS, andradar instruments on the Cassini spacecraft. It may episodically be released to theatmosphere, as recently suggested by Tobie and coworkers (2005). In any case, themethane cycle should indeed produce large amounts of complex organics accu-mulating on the surface as well as large amounts of ethane, which, when mixedwith the dissolved atmospheric methane, should form liquid bodies on the surfaceor in the near subsurface of the satellite. Maybe the dark feature seen near Titan’ssouth pole (Fig. 9.14) represents one of these expected liquid bodies.From the current data, Titan looks like another world, with an active prebiotic-

like chemistry but a lack of permanent liquid water on its surface. For this reason,Titan represents a natural planetary laboratory for prebiotic-like chemistry.The Cassini–Huygens mission is still proceeding. It will continue its systematic

exploration of the Saturnian system up to 2008, and probably to 2011 if theextended mission is accepted. Numerous data of paramount importance for astro-biology are still expected from several of its instruments (Table 9.3). The CIRSinstrument should be able to detect new organic species in the atmosphere duringfuture limb observations of Titan, especially at the pole. ISS and VIMS shouldprovide more-detailed pictures of Titan’s surface revealing the complexity and even

9 Astrobiology of Saturn’s Moon Titan248

Fig. 9.14 Picture of Titan taken near the southpole (cross in the middle) by the ISS narrow-angle camera on Cassini. It shows, in addition tobright clouds, the presence of a dark feature onthe upper left, which may be interpreted as aliquid hydrocarbon lake (image credit: NASA/JPL/Space Science Institute).

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the physical and chemical nature of this surface and its diversity. Radar observationwill continue the systematic coverage of Titan’s surface, showing contrastedregions with smooth and rough parts that suggest shorelines. Observations ofthe same regions with these instruments coupled with those already performedwith other instruments should bring a fruitful synergy (Fig. 9.15). In the longerterm, future missions to Titan, including horizontal mobility to explore the surfacein great detail and to analyze it at the molecular level and at many differentlocations, are already being considered. Such projects, if implemented, mightbring essential information for our understanding of this astrobiological, exotic,and astonishing world.

9.7Further Reading

9.7.1Books and Articles in Books

Gargaud, M., Barbier, B., Martin, H., Reisse,J. (Eds.) Lectures in Astrobiology, Vol. 1,Springer, Heidelberg, 2005.

Harland, D.M. Mission to Saturn, Cassini andthe Huygens Probe, Springer-Praxis Pub.,Chichester, UK, 2002.

Lacoste H (Ed.), Proceedings of the SecondEuropean Workshop in Exo-Astrobiology,Graz, Austria, 16–19 September 2002, ESASP 518, ESA-ESTEC, Noordwijk, The Neth-erlands, 2002, with the following articles:• Abbas, O., Schulze-Makuch, D. Acetylene-based pathways for prebiotic evolution onTitan, ESA SP-518, 2002, pp. 345–348.

• Bernard, J.-M., Coll, P., Raulin, F. Variationof C/N and C/H ratios of Titan’s aerosolsanalogues. ESA SP-518, 2002, pp. 623–625.

Lorenz, R., Mitton, J. Lifting Titan’s Veil- Ex-ploring the Giant Moon of Saturn, CambridgeUniversity Press, Cambridge, UK, 2002.

Russell, C. T. Cassini-Huygens Mission: Over-view, Objectives and Huygens Instrumenta-rium, Kluwer Academic Publishers, Dor-drecht, The Netherlands, 2003.

Russell, C. T. The Cassini-Huygens Mission:Orbiter Remote Sensing Investigations, KluwerAcademic Publishers, Dordrecht, TheNetherlands, 2005.

9.7 Further Reading 249

Fig. 9.15 One of the largest impact craters(about 80 km in diameter) observed on Titan’ssurface by two Cassini instruments: VIMS infra-red (left) and VIMS false-color image (right) andradar image (center). The faint halo, slightlybluer and darker than the surrounding parts, is

probably somewhat different in composition.Because it is made of material excavated whenthe crater was formed, this indicates that thecomposition of Titan’s upper crust varies withdepth (image credit: NASA/JPL/University ofArizona).

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Schulze-Makuch, D., Irwin, L. N. Life in theUniverse. Expectations and constraints, Spring-er, Berlin, Heidelberg, New York, 2004.

Simakov, M. B. The possible sites for exobio-logical activities on Titan, in: Proceedings of

the First European Workshop on Exo-/Astro-biology, Fracati, Italy, 21–23 May 2001,Ehrenfreund, P., Angerer, O., Battrick, B.(Eds.) ESA SP-496, ESA-ESTEC, Noordwijk,2001, pp. 211–214.

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9.7.2Articles in Journals

Artemieva, N., Lunine, J. Cratering on Titan:impact melt, ejecta, and the fate of surfaceorganics, Icarus 2003, 164, 471–480.

Bernard, J.-M., Coll, P., Coustenis, A., Raulin, F.Experimental simulation of Titan’s atmos-phere detection of ammonia and ethyleneoxide, Planet. Space Sci. 2003, 51, 1003–1011.

Coll, P., Coscia, D., Smith, N., Gazeau, M. C.,Ramirez, S. I., Cernogora, G., Israel, G.,Raulin, F. Experimental laboratory simula-tion of Titan’s atmosphere: aerosols and gasphase, Planet. Space Sci. 1999, 47 (10–11),1331–1340.

Fortes, A. D. Exobiological implications of apossible ammonia-water ocean inside Titan.Icarus 2000, 146, 444–452.

H�brard, E., Benilan, Y., Raulin, F. Sensitivityeffects of photochemical parameters uncer-tainties on hydrocarbon production in theatmosphere of Titan, Adv. Space Res. 2005,36 (2), 268–273.

Imanaka, H., Khare, B. N., Elsila, J. E., Bakes,E. L. O., McKay, C. P., Cruikshank, D. P.,Sugita, S., Matsui, T., Zare, R. N. Laboratoryexperiments of Titan tholin formed in coldplasma at various pressures: implications fornitrogen-containing polycyclic aromaticcompounds in Titan haze, Icarus 2004, 168,344–366.

Mousis, O., Gautier, D., Bockel�e-Morvan, D.An evolutionary turbulent model of Saturn’s

subnebula: Implications for the origin ofthe atmosphere of Titan, Icarus 2002, 156,162–175.

‘The Huygens probe on Titan’, News & Views,Articles and Letters, Nature 2005, 438, 756–802.

Prinn, R. G., Fegley, B. Kinetic inhibition ofCO and N, reduction in circumplanetarynebulae: implications for satellite composi-tion, Astrophys, J. 1981, 249, 308–317.

Raulin, F. Exo-astrobiological aspects of Euro-pa and Titan: from observations to specula-tions, Space Sci. Rev. 2005, 116 (1–2), 471–496.

Sekine, Y., Sugita, S., Shido, T., Yamamoto, T.,Iwasawa, Y., Kadono, T., Matsui, T. The roleof Fischer–Tropsch catalysis in the origin ofmethane-rich Titan, Icarus 2005, 178, 154–164.

Tian, F., Toon, O. B., Pavlov, A.A, De Sterck, H.A Hydrogen-rich early Earth atmosphere,Science 2005, 308, 1014–1017.

Tobie, G., Grasset, O., Lunine, J. I., Mocquet,A., Sotin, C. Titan’s internal structure in-ferred from a coupled thermal-orbitalmodel, Icarus 2005, 175, 496–502.

Wilson, E. H., Atreya, S. K. Current state ofmodeling the photochemistry of Titan’smutually dependent atmosphere and iono-sphere, J. Geophys. Res. – Planets 2004, 109(E6), E06002.

9.7.3Web Sites

NASA web site on Cassini mission:http://www.jpl.nasa.gov/cassini/

ESA web site on Huygens probe:http://sci.esa.int/huygens/).

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9.8Questions for Students

Question 9.1Given the surface temperature (94 K) and pressure (1500 hPa = 1.5 bar) of Titan,

determine the relative density of its atmosphere near the surface compared to thatof the Earth.Question 9.2(a) From the period of Saturn around the sun (29.4 years), deduce the mean

distance of Titan from the Sun. (b) From the mean distance of Titan from the Sundetermined in (a), determine the mean solar flux received at Titan compared to theEarth.Question 9.3 (see Figs 9.16 and 9.17)In Titan’s atmosphere the main product of methane photochemistry is ethane,

via the following reaction:

CH3 + CH3 + M� C2H6 + M,

where M is a third body.(a) This reaction does not occur in the high atmosphere of Titan. Why not? (b) In

the low atmosphere, CH3 radicals cannot be directly produced by methane pho-tolysis, but C2H and C4H radicals are directly produced by acetylene and diacety-lene photolysis. Why? (c) Give the mechanism of formation of CH3 radicals inTitan’s stratosphere photocatalyzed by acetylene. (d) Give the mechanism offormation of CH3 radicals in Titan’s stratosphere photocatalyzed by diacetylene.

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Fig. 9.16 UV spectra of methane, acetylene, and diacetylene.

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Question 9.4Knowing

• the scale height of Titan’s troposphere: Ha = 22 km,• the surface pressure: Ps = 1.5 � 105 Pa,• the mean mole fraction of methane in the troposphere:

fm = 0.03,• the global flux of destruction of methane in the atmosphere:

� = 1010 molecules/cm–2 s–1, and• the value of the Boltzman constant: kb = 1.4 � 10–23 J/K,

determine how long it will take for the whole atmospheric methane to disappear, inthe absence of any source on Titan. What suggests this value?Question 9.5Methane does not absorb in the visible. Its UV and IR spectra are given in Figs

9.16 and 9.17. Explain why methane produces a greenhouse effect in Titan’satmosphere.

9 Astrobiology of Saturn’s Moon Titan252

Fig. 9.17 IR spectrum of methane.

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10Jupiter’s Moon Europa: Geology and HabitabilityChristophe Sotin and Daniel Prieur

After reviewing the current knowledge of the geological processesand the surface composition of Jupiter’s moon Europa, this chapterconcentrates on the geophysical data that suggest below the icecrust the presence of a deep ocean that would be in contact with asilicate core. Models of Europa’s thermal evolution are then de-scribed. Based on the ocean hypothesis of Europa, the chapter thenconsiders the astrobiological aspects of Europa and the perspec-tives of potential life at the interface between the ocean and thesilicate core. Reference is given to the adaptability of terrestrial lifeto extreme environments. As outlook, some experiments are de-scribed that could be carried out onboard future missions to theJupiter system and its moon Europa in order to resolve some of theimportant issues related to putative habitability in the outer SolarSystem.

10.1A Short Survey of the Past Exploration of Europa

The four largest moons of Jupiter – Io, Europa, Ganymede, and Callisto – werediscovered in 1610 by Galileo Galilei, who used a self-made telescope. He recog-nized the importance of the Jupiter moons in supporting Kepler’s conception ofthe Sun being the central body in our Solar System; therefore, in his honor, thesefour moons are now called the Galilean satellites. At nearly the same time (actuallya few weeks earlier), the four moons were discovered by Simon Marius, a Germanastronomer, who gave them the names of the favorites of the ancient chief godJupiter, except for Ganymede, who was the cupbearer of the gods.Europa is the second Galilean satellite with regard to its distance to Jupiter. It

orbits around Jupiter at a period of 3.55 days (Table 10.1). Its orbit is controlled bythe so-called (1,2,4) Laplace resonance between Io, Europa, and Ganymede thatmaintains an eccentricity on the order of 1%.

10.1 A Short Survey of the Past Exploration of Europa 253

Complete Course in Astrobiology. Edited by Gerda Horneck and Petra RettbergCopyright � 2007 WILEY-VCH Verlag GmbH & Co. KGaA, WeinheimISBN: 978-3-527-40660-9

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Table 10.1 Characteristics of Jupiter’s moon Europa.

Parameter Quantity and dimension

Radius 1 560 € 10 kmDensity 3 018 € 35 kg m–3

GM[a] 3 202.86 € 0.07 km3/s2

Gravity acceleration at the surface 1.31 m/s2

J2[b] 389 € 39 10–6

C/MR2[c] 0.347Period of rotation 3.55 daysDistance to Jupiter 0.6709 109 mMass of Jupiter 1.905 1027 kgEccentricity 0.96%

a G = gravitational constant, M = Europa’s mass.b J2 = constant (see Eq. (10.1)).c C = moment of inertia, R = Europa’s radius (see Radau formula, Eq. (10.6)).

The first images of themoon Europa came from theVoyagermissions, which reachedthe Jupiter system on 5 March 1979 at a distance of 349 000 km (Voyager 1) and on9 July 1979 at a distance of 722 000 km (Voyager 2), before advancing to Saturn,Uranus, and Neptune, and further towards the outer edge of the Solar System. TheVoyagermissionswere designed to take advantage of a rare geometric arrangement ofthe outer planets in the late 1970 s and the 1980 s that allowed for a four-planet tour ata minimum of propellant and trip time. The images of Europa obtained by Voyager 2showed a smoothness of most of the terrain and the near absence of impact craters.Only three craters larger than 5 km in diameter have been found.But most of the information about Europa comes from the Galileo mission,

which orbited around Jupiter from 8 December 1995 until 28 September 2003. Thehigh-resolution images revealed intriguing tectonic features, such as domes, dis-rupted blocks, chaotic terrains, and fractures (Figure 10.1). The small number ofimpact craters suggests that Europa’s surface has undergone some kind of resur-facing by tectonic and/or cryovolcanic processes.

10 Jupiter’s Moon Europa: Geology and Habitability254

Figure 10.1 High-resolution image of theice-rich crust of Jupiter’s moon Europa, taken bythe solid-state imaging system on board theGalileo spacecraft on 20 February 1997, from adistance of 5 340 km during the spacecraft’sclose flyby of Europa. The area shown is about34 km by 42 km, centered at 9.4 degrees northlatitude, 274 degrees west longitude, and theresolution is 54 m (Photo credit: NASA/JPL).

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From an astrobiology point of view, the most interesting feature of Europa is theexistence of a putative ocean of water. Life on Earth cannot exist without liquidwater, which represents the major content of all known living organisms. Althoughcertain organisms can form highly dehydrated resting stages–for example, spores,cysts, or seeds–that allow them to survive unfavorable environmental conditions(see Chapter 5), these organisms cannot carry out their whole life cycle in theabsence of liquid water, which is needed at least for some time to allow metabolismand growth. Consequently, places in the Solar System where liquid water exists areconsidered potential targets for astrobiology investigations (see Chapter 6).Among the four Galilean satellites, Europa is not the only body possibly harbor-

ing a significant volume of liquid water. But according to the models, Europarepresents a single case in which liquid water is in contact with a silicate core (seealso Chapter 9, Figure 9.1), whereas for Ganymede and Callisto the water layer issupposed to be encased between layers of ice. These unique conditions on Europawould allow chemical exchanges between the ocean and the rocks of the core,thereby providing to this environment a variety of chemicals that might play a rolein sustaining putative life forms on the ocean floor. A similar situation exists onEarth in deep-sea hydrothermal vents, which are known for being inhabited byluxuriant communities of different types of organisms (see Chapter 5).

10.2Geology of the Moon Europa

10.2.1Surface Features

The images acquired by the Galileomission show very intriguing tectonic features,including domes, disrupted blocks, and fractures. Crustal plates ranging up to13 km across have been broken apart and “rafted” into new positions (Figure 10.1).They superficially resemble the disruption of pack ice on polar seas during springthaws on Earth. The size and geometry of those features suggest that motion wasenabled by ice-crusted water or soft ice close to the surface at the time of disruption.These disrupted blocks, also called “rafts,” have been interpreted by two different

models. Onemodel explains the formation and displacement of blocks as the resultof a thin, icy crust (less than 2 km) above an ocean (Figure 10.2). The thin crust isperiodically broken by faults that form in response to the tidal forces resulting fromEuropa’s eccentric orbit around Jupiter. The blocks resulting from the faulting ofthe ice crust would then be entrained by the streams of the liquid ocean and moverelative to each other. Because the surface temperature of about 100 K is muchbelow the freezing point, the displacement of the blocks would be limited by therapid freezing of any liquid that would be present between the blocks. Anotherreason for the crust to be disrupted is the possibility of localized sources of heat inEuropa’s silicate layer. It has been proposed that tidal forces would lead to partialmelting in Europa’s silicate layer and volcanism at the silicate–water interface. This

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scenario is inspired by the one that has been proposed in order to explain Io’s veryactive volcanism. In this case, the water would be very hot during a volcaniceruption and would rise to the surface, melting the ice crust and inducing strongdisplacements. It must be noted that volcanism is not necessarily required for thisprocess. Convection in Europa’s silicate layer would create zones of higher temper-ature, and percolation of water within the silicates would create conditions favor-able for hydrothermalism and subsequent displacement of hot water to the surface.Such a scenario is appealing to astrobiology, because the conditions at the silicate–ocean interface are very similar to those existing at several places on Earth’sseafloors.An alternative model assumes that the blocks and domes are related to sub-

solidus (solid-state) convection in the lower part of the crust (Figure 10.3). In thismodel, the domes are explained by the topography resulting from the rising of hotsubsolidus icy plumes forming at the interface between the liquid layer and the icycore. It strongly suggests subsolidus convection in the icy crust. The topography ofthe domes is not well constrained and cannot be used to constrain the character-istics of the upwelling plumes. If this is the right explanation for the domes, itimplies that the thickness of the ice crust is at least 20 km.Europa’s surface is covered by very long fracture zones, which were observed by

the Voyager mission. Tidal forces driven by Jupiter have been supposed to beresponsible for the formation of those cracks. Some cracks form chains of arcsthat are connected at the cusps. Those cycloidal cracks might be formed inresponse to diurnal variations of the tidal forces.The low number of impact craters suggests that Europa’s surface is young

compared to that of the Galilean satellites Ganymede and Callisto. However, it isdifficult to obtain absolute ages of surfaces from the number of impact craters,

10 Jupiter’s Moon Europa: Geology and Habitability256

Figure 10.2 “Raft” model to explain the surface structuresof Jupiter’s moon Europa with hot water rising from theocean-silicate interface (from Thomson and Delaney 2001).

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because the cratering rate in the outer Solar System is not well known. Modelssuggest an age of between 10 million years and one billion years for the surface ofEuropa. Another possibility for assessing the age is the erosion rates by sputtering.However, these estimates are constrained by the measurements of the H2O escaperate during the Galileomission. If the sputtering has been operating for more thanone billion years, it should have erased most of the topography; however, this is notthe case for Europa. The remaining topography of Europa is consistent with an ageof its surface in the range of some million years.There are also a few multi-ringed structures on Europa, such as Tyre and

Callanish, which are interpreted as impact features. Study of the topographicrelaxation of those fractures suggests a low viscosity layer at about 5–10 km indepth. This layer may be either a liquid layer or a soft ice layer. This interpretationof the formation and relaxation of impact craters may be the strongest argument infavor of a deep liquid ocean below an icy crust.The spacecraft Galileo finally plunged into Jupiter’s crushing atmosphere on 21

September 2003. The spacecraft was deliberately destroyed for planetary protectionreasons (see Chapter 13). The aim was to avoid a potential crash of the spacecraftwith the moon Europa, in order to protect the possible ocean beneath the icy crustfrom terrestrial contamination.

10.2.2Composition of the Surface

Data from the near-infrared mapping spectrometer (NIMS) onboard the Galileospacecraft show that Europa’s surface is made mostly of water ice. In order toexplain the spectra obtained along the cracks, another component must exist inaddition to water. It has been proposed that this additional component be hydratedmagnesium sulfate. Such material might have been released by some kind ofcryovolcanic activity related to the activity of the cracks.

10.2 Geology of the Moon Europa 257

Figure 10.3 Subsolidus convection model for explaining thechaotic terrains and the displacement of blocks on Europa’ssurface (modified from Sotin et al. 2002).

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10.3Internal Structure of the Moon Europa

The density of Europa, at 3 018 kg m–3 (Table 10.1), lies between that of Io(3 530 kg m–3) and that of Ganymede (1 936 kg m–3) and Callisto (1 851 kg m–3).Because its surface is made of water ice, Europa is likely composed of a mixture ofwater ice and silicates. Taking Io’s density for the density of silicates and a value of960 kg m–3 for H2O (the latter value is assumed to lie between that of liquid water[1 000 kg m–3] and that of iceI [920 kg m–3]), the mass fraction of ice on Europawould be only 6%. Another way to interpret the density data is that Europa wouldbe made of a rocky core of 1 450 km in radius overlain by a 110-km thick layer ofH2O (Figure 10.4).Additional information about the internal structure of Europa comes from

magnetic and geodetic measurements during the Galileo mission. Europa has astrong inductive magnetic field consistent with an electrically conducting interiorwith a radius equal to nearly the entire radius of the moon. However, it does notshow any evidence of a permanent dipole. The induction field can be explained by awater ocean of similar conductivity to the Earth’s oceans, provided this ocean has athickness exceeding 10 km (Figure 10.4). One must note that another explanationis the existence of an iron core. At the present time, it is not possible to choosebetween these two options, because the depth of the induced magnetic field cannotbe determined.The gravity potential was measured during the 11 Europa flybys of the Galileo

mission. The gravity potential can be expressed in spherical harmonics decom-position. For flybys such as those realized during the Galileomission, only degrees0 (GM/r) and 2 are kept. The relation is as follows:

10 Jupiter’s Moon Europa: Geology and Habitability258

Figure 10.4 Internal structure of Jupiter’smoon Europa deduced from line-of-sightmeasurements and magnetic field measure-ments during the Galileo mission.

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U ¼ GMr

1þ aer

� �2�J2P2;0ðsinðºÞÞ þ J2;2 cosð2çÞP2;2ðsinðºÞÞ� �� �

(10.1),

where U is the gravity potential, G is the gravitational constant, M is Europa’smass, r is the distance to the center of mass (CoM), ç is longitude, º is latitude, ae isthe equatorial radius, J2 and J2,2are constants to be determined, and P2,0 and P2,2 areassociated Legendre polynomials. Assuming hydrostatic equilibrium, the J2 valueis related to the hydrostatic Love number kS and the periodic Love number k2 by thefollowing equations:

J2 = J2h + ˜J2 = (1/2 Æ + 1/3 q) kS + 3/2 Æ k2e cos (�) (10.2)

J2,2 = J2,2h + ˜J2,2 = 1/4 Æ kS + 3/4 Æ k2e cos (�) (10.3),

where J2h and J2,2h are the hydrostatic parts of the degree 2 coefficients of Eq. (10.1).In Eqs. (10.2) and (10.3), e is the eccentricity and � is the true anomaly. Thecoefficients Æ and q are defined by

Æ ¼ M�

M� R

D

� �3

(10.4)

and

q ¼ ø2R3

GM(10.5),

whereM� is Jupiter’s mass, D is the mean distance between Europa and Jupiter, Ris Europa’s radius, and ø is the rotation period.Unfortunately, the flybys did not have a geometry that allowed J2,2 to be deter-

mined. Assuming hydrostatic equilibrium, J2,2 is equal to 0.3 J2. With this assump-tion, it is not possible to determine the value of the periodic Love number k2. Then,the hydrostatic Love number kS is related to the moment of inertia C about therotation axis by the Radau formula:

CMR2

¼ 23

1� 25

ffiffiffiffiffiffiffiffiffiffiffiffi4� ks1þ ks

s !(10.6).

Assuming a one-dimensional model (density depends only on radius), the momentof inertia can be calculated for a given internal structure by the following equation:

C ¼Z

Mx2dm ¼ 8�

3

Z R

0æðrÞr4dr (10.7),

where x is the distance of every elementary mass dm to the axis and æ is the densitythat depends on radius (r). In order to build an internal model of Europa, it has

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been assumed that the density depends only on the material that composes thelayer. The variations due to temperature and pressure are negligible compared tothose induced by the change of material.Assuming that the massM of a celestial body is known, the determination of the

moment of inertia provides a relationship between the size of the core, its density,and the density of the H2O mantle in a model where there are only two layers.However, the value found for Europa suggests that an iron core must be present. Itis consistent with a fully differentiated moon that includes an inner iron-rich core(Figure 10.4).It must be noted that the presence of an ocean strongly modifies the value of k2

(Figure 10.5). Such a measurement of k2 may become possible in a future missionto Europa, if the spacecraft orbits around Europa.

10.4Models of Evolution of the Moon Europa

With the progress made in modeling thermal convection in planetary interiors,models describing Europa’s thermal evolution have substantially improved in thelast 20 years. Important improvements include the description of convection forcomplex viscosities by Deschamps and Sotin and information on the couplingbetween orbital characteristics and tidal heating by Tobie and coworkers. Heatsources include the heat of accretion, the heat produced by the decay of long-livedradiogenic elements, and tidal heating. The amount of tidal heating depends on theviscosity (Figure 10.6). The curve in Figure 10.6 has a bell-like shape with a

10 Jupiter’s Moon Europa: Geology and Habitability260

Figure 10.5 Variation of the periodic Love number k2 for modelswith a deep ocean or without an ocean (from Castillo et al. 2000).

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maximum viscosity around 1014 Pa s, which is the viscosity of ice close to itsmelting point. The amount of tidal heating is much larger for Europa than thatfor the two Galilean satellites Ganymede and Callisto or for Saturn’s moon Titan. Itmay be more than an order of magnitude larger than radiogenic heating.The first studies of the internal structure and thermal evolution of icy satellites

were conducted prior to the Voyagermission in the late 1970 s by Consolmagno andLewis. Subsolidus convection was not considered in those studies, and heatproduced by the decay of radiogenic elements contained in a differentiated silicatecore was supposed to be transferred by conduction. In a one-dimensional model,the surface heat flux (qS) is proportional to the temperature gradient (�T/�r)z=0 asfollows:

qS ¼ Q4�R2

¼ k@T@r

� �

z¼0(10.8),

where Q is total power and k is the thermal conductivity that depends on temper-ature (Table 10.2). The thickness of the ice crust can be estimated very simply if onemakes the following assumptions:

• there is no heat production in the ice crust,• thermal conductivity does not depend on temperature,• there is equilibrium between the radiogenic heating rate and

the total heat power released, and• the melting temperature is that of pure H2O.

Table 10.2 Thermal properties of ice and silicates.

Silicate Ice Mixture of ice and silicates[a]

Thermal conductivity(k in W/m/K)

4.2 0.4685 + 488.12/T fs · kS + (1 – fs) · kI

Heat capacity (C in J/kg/K) 920 185 + 7.037/T xs · CS + (1 – xs) · CI

a Index S stands for silicate, index I for ice.

10.4 Models of Evolution of the Moon Europa 261

Figure 10.6 Amount of tidal heating versusviscosity for the three Galilean satellites Europa,Ganymede, and Callisto and for Saturn’ moonTitan; the horizontal lines represent the amountof radiogenic power at present time in eachsatellite for comparison with tidal heating (fromSotin and Tobie 2004).

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These assumptions lead to a present heat flux around 8 mWm–2, which provides athickness of the ice crust of about 50 km. Subsequent studies by Deschamps andSotin showed that the ice layer would be unstable to convection for such largevalues of the ice crust thickness.Up to the mid-1990 s, thermal convection models were calculated using isovis-

cous scaling laws. Recent progress in the modeling of thermal convection proc-esses for fluids having complex viscosity has changed the scaling laws that onemust apply in order to investigate the cooling rate of a planet. If one ignores thepossibility of tidal heating, the ice crust can be modeled as a viscous fluid boundedby two isothermal boundaries: the surface (T = 100 K) and the ocean (T = Tm). Inthe case of a fluid with only temperature-dependent viscosity, numerical simula-tions and laboratory experiments suggest that the amount of heat that can betransferred by subsolidus convection is driven by the instabilities, which form inthe lower (hot) thermal boundary layer. Once stationary convection is reached, thethermal boundary layer is characterized by a constant value of the thermal boun-dary layer Rayleigh number (RaTBL) as follows:

RaTBL ¼ÆægðTm � TiceÞ�3

Œ�(10.9),

where � is the thickness of the thermal boundary layer, Æ is the coefficient ofthermal expansion, � is ice viscosity, Œ is thermal diffusivity, and Tice is thetemperature of the convective ice layer, which is the layer located between thetwo thermal boundary layers. The temperature difference (Tm – Tice) across thethermal boundary layer is proportional to a viscous temperature scale (˜T�):

Tm � Tice ¼ 1:43˜T� ¼ 1:43�1

@Lnð�Þ=@T� �

T¼Tice

0B@

1CA (10.10).

If one knows how ice viscosity depends on temperature, then one can calculate thetemperature difference across the thermal boundary layer. Heat flux can becalculated using a law similar to Eq. (10.8):

q ¼ Q4�R2

m

¼ kTm � Tice

� �(10.11),

where � is the TBL thickness determined by Eq. (10.9) and Rm is the radius of theliquid–ice interface. Viscosity of ice is the key parameter controlling the amount ofheat that can be transferred by subsolidus convection. Taking values of 1014 Pa s forthe viscosity of ice at its melting point and activation energies of 50 kJ per moleleads to a freezing of the ocean in less than one billion years for a simple modelignoring tidal dissipation.If tidal dissipation is taken into account, it happens mostly in the convective layer.

Because the total amount of heat is controlled by the instability in the top cold

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boundary layer, the heat flux at the base of the icy crust is limited to the differencebetween surface heat flux and tidal dissipation. This small heat flux prevents Europafrom freezing completely. Tidal heating in a convective shell explains the presence ofan oceanwithin Europa without invoking the presence of antifreezematerial such asammonia. The silicate core may eventually heat up if not enough heat can beremoved through the ice layer. Another interesting feature related to tidal heating,as proposed by Sotin’s group, is localized heating in upwelling plumes leading topartial melting of ice. Because liquid H2O is denser than ice, it creates a depressionthat may explain the chaotic terrains (Figure 10.3). It also generates a negativebuoyant force that prevents liquids from migrating to the surface.The thickness of Europa’s ice shell may be subject to changes with time, adjust-

ing to the decrease in radiogenic heat and, more importantly, to variations in tidaldissipation that depend on orbital eccentricity. Although the amount of tidalheating depends on the thickness of the ice shell, creating a buffering effect onthickness variations, an important consequence of such a thermal-orbital couplingis that the thickness of Europa’s ice shell may vary between a few kilometers and afew tens of kilometers on a time scale on the order of 100 million years. Theobserved diversity of geological surface features on Europa also may be due to thesetime-dependent variations of ice thickness.

10.5Astrobiological Considerations about Possibilities for Life on the Moon Europa

Astrobiology aims at studying the origin, distribution, and evolution of life in theUniverse. The major issue is that we, inhabitants of the Earth, only know life onour planet. For this reason, the search for life elsewhere in the Universe, and moresimply in our Solar System, uses life on Earth as a reference (see Chapter 6). In thischapter, the knowledge about life on Earth is used for asking the followingquestions: Is or was there life on Europa and, if the answer is yes, why? In thisstudy, only small-sized organisms, namely, microorganisms, will be considered,because early life forms on Earth also were admittedly represented by microorgan-isms (see Chapter 4). However, it is muchmore difficult to detect suchmicroscopiclife than large-sized organisms; their detection would probably not be a problem.There are plenty of definitions for life on Earth, and this point could be the

central theme of several books (see Chapter 1). More simply, all organisms livingon Earth are organized on either a cellular basis–i.e., all animals, plants, andmicroorganisms–or a non-cellular basis–i.e., viruses and prions. All life formsare complex assemblages of atoms, particularly C, N, H, O, P, S, K, Mg, Na, Ca,and Fe, which constitute the macronutrients. These macronutrients form macro-molecules (proteins, lipids, polysaccharides, and nucleic acids), which all containcarbon, are solved in water, and are present in all living forms. Water represents anideal biological solvent, because of its polarity and cohesiveness; it is a necessaryprerequisite for life as we know it. Briefly, life requires, at the very least, liquidwater and carbon.

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It is now generally accepted that liquid water may exist on Europa. Therefore, thefollowing question now needs to be discussed: What else is required for life?Still considering life on Earth as a reference, one can infer that all cellular and

non-cellular organisms contain at least proteins, which are polymers of aminoacids, each made of C, H, O, and N (see Chapter 3). Carbon is the major elementpresent in large concentrations in all living forms, and one cannot raise thequestion of life on Europa without addressing the availability of carbon. Livingforms on Earth use relatively simple carbon-containing molecules as a startingpoint to synthesize macromolecules. The carbon source can be carbon dioxide(inorganic) and other C1 compounds (molecules containing only one atom ofcarbon, such as CO or CH4) or organic carbon (consisting of one or more carbonatoms associated with H, O, and N, such as sugars, aldehydes, alcohols, fatty acids,amino acids, etc.).Although the surface of the ice crust of Europa has been rearranged (and this is

one of the arguments in favor of a liquid water ocean beneath the ice crust), a fewimpact craters (caused by meteorite impacts) are still visible. Taking into accountthe analysis carried out in many laboratories about the chemical composition ofmeteorites delivered to Earth (see Chapter 3), there is no doubt that organic carbonhas been delivered to Europa, and probably in rather large amounts, especially ifone considers the numerous impacts visible on Io, another Galilean satellite.Likewise, on early Earth, carbon and other atoms essential for life were deliveredthrough meteorite bombardments.At this step of considerations, all major ingredients for life are theoretically

present on Europe. But is that enough? Considering again life on Earth, cellularorganization prevails, and non-cellular organisms (viruses and prions) depend on acellular host for their replication. A cell is an entity enclosed in a semipermeablemembrane, which isolates the cell from its environment (including other cells) butallows exchange of material with this environment (in both directions, in and out).These materials include nutrients and particularly carbon sources but also energysources (see Chapter 5).What energy sources are used on Earth by living organisms? The two main

energy sources are light energy from the Sun and chemical energy. Light emittedby the Sun may be converted into chemical energy: it is mostly used for the fixationof carbon dioxide and its conversion into organic carbon through photosynthesis.This process is used by plants, seaweeds, microalgae, and some bacteria.The other energy source is of a chemical nature and is based on the transfer of

electrons from a reduced compound (electron donor) to an oxidized compound(electron acceptor). Both the electron donor and the acceptor are taken by the cellsfrom their surrounding environment. The electron transfer from the donor to theacceptor takes place within the cell membrane and is accompanied by an extrusionof protons. This leads to the formation of a gradient of protons across themembrane, with more protons outside than inside. This gradient or proton motiveforce is catalyzed by a specific enzyme, ATPase, which uptakes protons fromoutside to inside and forms ATP (adenosine triphosphate), a highly energeticmolecule.

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On Earth, there is a huge diversity of electron donors and acceptors that can beused by living organisms, provided they have the suitable set of enzymes, forexample, electron carriers. Animals use organic molecules as electron donors andmolecular oxygen as electron acceptor. But microorganisms are more versatile andmay use hydrogen, sulfur, hydrogen sulfide, ammonium, nitrite, or ferrous iron aselectron donor, while the electron acceptor may be carbon dioxide, sulfur, sulfate,nitrate, or ferric iron, depending on the reduction potential of the compoundconsidered. It should be noted that molecular oxygen is not involved in thesestrictly anaerobic reactions, although molecular oxygen is an excellent electronacceptor that is used when it exists but is not a prerequisite for life. Indeed, lifestarted on Earth well before photosynthetic organisms appeared that eventuallyreleased oxygen into the environment.What kind of energy sources might be available on Europa? They might come

from outside of the moon by meteorites or from its interior. The latter point will beconsidered in the following. As pointed out in Section 10.3, among the Galileansatellites that probably harbor an ocean of liquid water, Europa represents a singlecase where the ocean is in contact with the silicate core. If the temperature of thecore is high and reaches up to its surface, then these conditions might foster theformation of hydrothermal circulations.On Earth, such hydrothermal vents have been discovered since 1977 in many

places of the oceans and particularly along oceanic ridges. In these tectonicallyactive areas, seawater penetrates through cracks of the seafloor and approaches themagma chamber. At elevated temperatures, seawater interacts with the rocks. Thisleaching process enriches seawater with various inorganic compounds such ashydrogen, hydrogen sulfide, carbon monoxide, carbon dioxide, methane, and othersmall molecules. After a complex circulation, the hot fluid eventually vents out.This fluid is different from seawater because it contains various new chemicals,and it is lighter than seawater because density decreases with temperature. From abiological point of view, it is noteworthy that this fluid delivers into the ocean aplume of chemicals that may serve as electron donors and acceptors. A variety ofmicroorganisms, Bacteria and Archaea (see Chapter 5), utilize these compoundsfor their energy metabolism and thrive optimally at those deep-sea hydrothermalvents. Furthermore, it has been proposed that some organic synthesis might occurunder hydrothermal conditions through Fischer-Tropsch reactions, thereby pro-viding an additional source of organic carbon (see Chapter 3).At this point of the considerations, one may anticipate that the moon Europa

might possess the major requirements for life, namely, liquid water, inorganic andorganic carbon, and chemical energy sources. Similar ingredients were also avail-able on the early Earth, when life started there (see Chapter 3). In the following, theputative environment of Europa is considered, and again life on Earth is taken asreference.Organisms on Earth are dependent on the physicochemical conditions of their

environment, in addition to the basic requirements of liquid water, carbon, andenergy sources. Major parameters of potential influence are temperature, salinity,pH, and hydrostatic pressure. Those parameters also may be relevant in the context

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of Europa. High intensities of ionizing radiations, generated by the intenseradiation belts of Jupiter, are also experienced at the surface of Europa, but becauseof the thickness of several kilometers of the ice crust, the ocean below is wellprotected from those radiations (Figure 10.7).The temperature of the upper layers of the Europan ocean, that is, the boundary

to the ice crust, should not be very different from 0�C, depending on the chemicalcomposition of the ocean; but it might be more elevated in the deepest parts,especially if the anticipated hydrothermal circulation exists. The salinity and pH ofthe ocean are also determined by its chemical composition. According to differentmodels, the Europan ocean is probably salty, and the pH may be either acidic oralkaline. Finally, because of Europa’s low gravity (Table 10.1), the depth of theocean of about 100 km would not result in a very high hydrostatic pressure at itsbottom. Pressures should not exceed 100 MPa.On Earth, environmental parameters as described above for Europa’s ocean are

compatible with those supported or even required by a group of organisms called“extremophiles” (see Chapter 5). Concerning temperatures, it is well known that atvery low temperatures macromolecules and even whole cells are preserved. Forinstance, gametes and embryos from mammals, seeds, or bacteria are commonlypreserved in liquid nitrogen at –196 �C. A temperature of –12 �C has been identifiedas the lower limit for growth of certain microorganisms isolated from permafrost;but many microorganisms, bacteria as well as algae, are still able to metabolize andgrow at temperatures close to 0 �C. At the top of the temperature scale, 113 �C is themaximum temperature for growth, as demonstrated by Pyrolobus fumarii, anArchaea isolated from a deep-sea hydrothermal vent. This organism grows opti-

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Figure 10.7 Rates of physically absorbed radiation doses, sepa-rate contributions of electrons and photons (bremsstrahlung), atthe surface of Jupiter’s moon Europa and below varying thick-nesses of ice (from Baumstark-Khan and Facius 2002).

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mally at 110 �C and is capable of surviving two hours in an autoclave underconditions that are commonly used for sterilization.Elevated salt concentrations, up to 5.5 M (for instance, 32% NaCl), still allow

growth of Archaea, which are called “extreme halophiles.” For optimal growththese organisms usually require concentrations of 1.5–4.0 M of salts, which corre-sponds to 9–23% NaCl. In many cases, Na+ ions constitute the brines, but Mg2+ orCa2+ ions also occur.With regard to pH values, acidophilic microorganisms grow at low pH and even

close to pH 0, for instance, the microorganism Picrophilus oshimae. Other bacteriaand algae are adapted to grow at pH values around 11. These are called “alka-liphiles.”The hydrostatic pressure of about 100 MPa that is anticipated to prevail at the

bottom of Europa’s ocean corresponds to the pressure in the deepest trenches ofEarth’s oceans, for instance, 110 MPa at 11 000 m depth. Microorganisms havebeen isolated from such high-pressure environments, and some microorganismsappear to require pressures of least 40 MPa to start growth.Considering the conditions that are expected for Europa’s ocean (i.e., the avail-

ability of liquid water and carbon and energy sources and the physicochemicalparameters), they are compatible with conditions that sustain life as we know it onEarth. These are arguments that justify proceeding with the search for life in thatdistant ocean. Of course, those conditions are still to be proven definitely, but theperspectives are a great challenge for future space missions to the Jovian systemand especially to its moon Europa.

10.6Summary and Conclusions

The discovery of an ocean on the Jovian moon Europa would be a major discoveryof planetary exploration. It will be a major step toward the questioning of habit-ability of satellites and planets and a first step to the question of life wherever thereis water. The results of the Galileo mission suggest that such an ocean may bepresent on Europa. However, each piece of evidence, taken separately, can beexplained without the presence of an ocean. The ocean hypothesis is also stronglysupported by models describing Europa’s thermal evolution and its relationshipswith surface features. Europa is unique among the icy satellites because the liquidH2O layer, if present, would be in contact with the silicate core. The conditions atthe core–ocean interface would be similar to those existing at the terrestrial oceanseafloor, where living organisms develop without using any solar energy. Althoughit is very tempting to imagine that Europa’s silicate core is volcanically active likethat on Io, recent calculations on tidal dissipation suggest that there is not enoughdissipation energy deposited in the silicate layer for silicates to reach their meltingpoint. The potential presence of liquid water and volcanism puts Europa on the listof possible life-bearing bodies, though the probability is very low. On the one hand,the presence of an ocean is very likely, but on the other hand, siliceous volcanic

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activity is not predicted by current models. We lack measurements that wouldprovide a definitive answer to these questions, and future missions will be devel-oped to acquire such data.

10.7Outlook and Plans for Future Missions

Jupiter’s moon Europa belongs to the family of icy satellites. Two features make itspecial in this family. First, the small amount of H2O makes possible an interfacebetween liquid water and a silicate core. Second, the Laplace resonance maintains ahigh eccentricity that is responsible for the large amount of tidal heating. Calcu-lations predict that tidal heating is mostly localized in the ice shell and that theamount is much larger than radiogenic heating. Tidal heating may prevent thetotal freezing of the satellite and would explain the presence of a liquid layer assuggested by the magnetic data. Europa may be the only place beyond Earth in theSolar System where a silicate–ocean interface exists. At this interface, conditionsare close to those existing on Earth’s seafloors. One important difference may bethe lack of silicate volcanism at this interface. The only argument for the absence ofvolcanism comes from numerical modeling. It would be important to acquire datathat can constrain such thermal evolution models.Several arguments exist in favor of space missions dedicated to the search for life

on Europa, and such a mission has been recommended to space agencies, partic-ularly by the U. S. Academy of Sciences and in Europe by several assemblies,including the European Astrobiology Network Association (EANA). Several sce-narios have been studied, from a simple orbiter to a lander including a cryobot,which is a vehicle able to reach the ocean and sample it after drilling 10 km throughthe ice crust. Novel data about Europa will obviously depend on the availabletechnology and associated costs.An orbiter mission to Europa should be able to map the surface with high

resolution, to determine the thickness of the ice crust, and to definitively prove(or disprove) the existence of an ocean. Additional data on the contact regionbetween the deep ocean and the core should be provided, as well as on the chemicalcomposition of the surface ice with regard to the occurrence of inorganics, organ-ics, and volatiles.Finally, a landing mission would provide contact access to the surface and would

allow ice sampling and analysis. However, because of the intense radiations at thesurface of Europa (Figure 10.7), it would be necessary to have access to the icesubsurface of 1–2 m to reach areas that are protected from radiations.Without a lander, it would still be possible to assess the presence of an ocean by

measuring the gravity potential and the variations of Europa’s equatorial radius asa spacecraft orbits around Jupiter (Figure 10.5). The thickness of the ice crust maybe more difficult to measure. A laser altimeter would measure the topography ofgeological features, which would allow geologists to better assess the time offormation of the different geological structures that pave Europa’s surface. Finally,

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infrared spectrometry and measurements of ions and neutrals along the orbitshould allow determination of both the molecular and the elementary compositionof the surface. Gravity potential measurements should allow determination oflateral mass variations in the silicate core if it has been subject to partial meltingand volcanism. Such information would be important for assessing the possibilityof life at the interface between the liquid layer and the silicate core.

10.8Further Reading

10.8.1Books and Articles in Books

Gargaud, M., Barbier, B., Martin, H., J. Reisse,J. (Eds.) Lectures in Astrobiology, Volume II,Springer, Berlin (in press), especially thefollowing chapter therein:– Prieur, D. An Extreme Environment onEarth: Deep-Sea Hydrothermal Vents.Lessons for Mars and Europa Exploration.

Greenberg, R. Europa, the Ocean Moon,Springer-Praxis, Chichester, UK, 2005.

Horneck. G., Baumstark-Khan, C. (Eds.) As-trobiology – The Quest for the Conditions ofLife, Springer, Berlin, 2002; especially thefollowing chapters therein:– Greenberg, R., Tuffs, B. R., Geissler, P.,Hoppa, G. V. Europa’s Crust and Ocean:How Tides Create a Potentially HabitablePhysical Setting, pp. 111–124.

– Stetter, K. O. Hyperthermophilic Micro-organisms, pp. 169–186.

– Baumstark-Khan, C., Facius, R., Lifeunder Conditions of Ionizing Radiation,pp. 261–284.

Jolivet, E., L’Haridon, S., Corre, E., G�rard, E.,Myllykallio, H., Forterre, P., Prieur, D. TheResistance to Ionizing Radiation of Hyper-thermophilic Archaea Isolated from Deep-Sea Hydrothermal Vents, in 1st European

Workshop on Exo/Astrobiology, 21–23 May2001, Frascati, Italy. Ehrenfreund, P., An-gerer, O., Battrick, B. (Eds.) ESA SP-496,ESA/ESTEC, Noordwijk, pp. 243–246, 2001.

Prieur, D. Deep-Sea Hydrothermal Vents: AnExample of Extreme Environment on Earth,in First Steps in the Origin of Life in the Uni-verse, Chela-Flores, J., Owen, T., Raulin, F.(Eds.) Kluwer Academic, Dordrecht, TheNetherlands. pp. 187–194, 2001.

Prieur, D., Voytek, M., Reysenbach, A. L. Jean-thon, C. Deep-Sea Thermophilic Prokar-yotes, in Thermophiles: Biodiversity, Ecologyand Evolution. Reysenbach, A.L, Voytek, M.,Mancinelli, R. (Eds.) Kluwer Academic/Ple-num Publishers, New York. pp. 11–22, 2001.

Prieur, D. Microbiology of Deep-Sea Hydro-thermal Vents: Lessons for Mars Explora-tion, in Water on Mars and Life, T. Tokano(Ed.), Springer, Berlin, pp. 299–324, 2005.

Reysenbach, A. L., Holm, N. G., Hershberger,K., Prieur, D., Jeanthon, C. In Search of aSubsurface Biosphere at a Slow-SpreadingRidge, in Proceedings of the Ocean DrillingProgram, Scientific Results, Vol. 158, Herzig,P.M., Humpris, S. E., Miller, D. J., Zieren-berg, R. A. (Eds.) pp. 355–360, 1998.

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10.8.2Articles in Journals

Brack, A., Ehrenfreud, P., von Kiedrowski, G.,Lammer, H., Prieur, D., Szuszkiewicz, E.,Westall, F. EANA trail guide in astrobiology:Search for a second genesis of life. Internat.J. Astrobiology, 2006, 4, 195–202.

Collins, G. C., Head, J.W., Pappalardo, R. T.,Spaun, N. A. Evaluation of models for theformation of chaotic terrain on Europa,J. Geohpys. Res. 2000, 105, 1709–1716.

Consolmagno,G.J., Lewis, J. S. The evolutionof icy satellite interiors and surfaces, Icarus,1978, 34, 280–293.

Deschamps F., Sotin C. Thermal convection inthe outer shell of large icy satellites, J. Geo-phys. Res. 2001, 106, 5107–5121.

Grasset, O., Parmentier, E.M. Thermal con-vection in a volumetrically heated, infinitePrandtl number fluid with strongly temper-ature-dependent viscosity: implications forplanetary thermal evolution, J. Geophys. Res.1998, 103, 171–181.

Hussmann H., Spohn T. Thermal-orbitalevolution of Io and Europa. Icarus, 2004,171, 391–410.

Khurana, K. K., Kivelson, M. G., Russell, C. T.Induced magnetic fields as evidence forsubsurface ocean in Europa and Callisto.Nature, 1998, 397, 777–780.

L�pez-Garcia, P., Moreira, D., Douzery, E.,Forterre, P., Van Zuilen, M., Claeys, P.,Prieur D. Ancient fossil record and earlyevolution (ca. 3.8 to 0.5 Ga), Earth MoonPlanets, 2006, 98, 247–290. DOI 10.1007/s11038–006–9091–9.

McCord, T. B., Hansen, G. B., Clark, R. N. Mar-tin, P. D., Hibbitts, C. A., Fanale, F. P., Gran-ahan, J. C., Segura, M., Matson, D. L., John-son, T. V., Carlson, R.W., Smythe, W.D.,Danielson, G. E., The NIMS Team, Non-water-ice constituents in the surface materialof the icy Galilean satellites from the Galileonear-infrared mapping spectrometer investi-gation, J. Geophys. Res. 1998, 103, 8603–8626.

McKinnon, W. B. Convective instability inEuropa’s floating ice shell, Geophys. Res.Lett., 1999, 26, 951–954.

Pappalardo, R. T., Head, J.W., Greeley, R.,Sullivan, R. J., Pilcher, C., Schubert, G.,

Moore, W. B., Carr, M.H., Moore, J. M.,Belton, M. J. S., Goldsby, D. L. Geologicevidence for solid-state convection in Euro-pa’s ice shell, Nature, 1998, 391, 365–368.

Pappalardo, R. T., Belton, M. J. S., Breneman,H.H., Carr, M.H., Chapman, C. R., Collins,G.C, Denk, T., Fagents, S., Geissler, P. E.,Giese, B., Greeley, R., Greenberg, R., Head,J. W., Helfenstein, P., Hoppa, G., Kadel,S. D., Klaasen, K. P., Klemaszewski, J. E.,Magee, K., McEwen, A. S., Moore, J. M.,Moore, W. B., Neukum, G., Phillips, C. B.,Prockter, L. M., Schubert, G., Senske, D. A.,Sullivan, R. J., Tufts, B. R., Turtle, E. P.,Wagner, R., Williams, K. K. Does Europahave a subsurface ocean? Evaluation of thegeological evidence, J. Geophys. Res., 1999,104, 24015–24055.

Pascal, R., Boiteau, L., Forterre, P., Gargaud,M., Lazcano, A., Lopez-Garcia, P., Maurel,M.-C., Moreira, D., Pereto, J., Prieur D.,Reisse J. Prebiotic chemistry – biochemistry– emergence of life (4.4–2 Ga), Earth MoonPlanets, 2006, 98, 153–203. DOI 10.1007/s11038–006–9089–3.

Smith, B. A. and the Voyager Imaging Team.The Galilean satellites of Jupiter, Voyager 2imaging science results, Science, 1979, 206,951–972.

Sotin C. Tobie G. Internal structure anddynamics of the large icy satellites, C. R.Acad. Sci. Physique, 2004, 5, 769–780.

Sotin C., Head J.W., Tobie G. Europa: Tidalheating of upwelling thermal plumes andthe origin of lenticulae and chaos melting,Geophys. Res. Lett. 2002, 29, 8, 74-1–74-4.

Thomson, R. E., Delaney, J. R. Evidence for aweakly stratified Europan ocean sustainedby seafloor heat flux, J. Geophys. Res., 2001,106, 12355–12365.

Tobie G., Mocquet A., Sotin C. Tidal dissipa-tion within large icy satellites: Europa andTitan, Icarus, 2005, 177, 534–549.

Zimmer, C., Khurana, K. K., Kivelson, M. G.Subsurface oceans on Europa and Callisto:Constraints from Galileo magnetometerobservations, Icarus, 2000, 147, 329–347.

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10.8.3Web Sites

http://www2.jpl.nasa.gov/galileo/europa/

10.9Questions for Students

Question 10.1Knowing Europa’s mass and assuming chondritic concentrations in radiogenic

elements, determine the heat power provided by the decay of radiogenic species. IfEuropa is neither cooling nor heating up, determine the heat flux at the surface.Determine the thickness of the ice layer if the melting temperature is 270 K and theheat conductivity described by k = 600/T where T is in K and k in W/m/K.Question 10.2Knowing the mass and the moment of inertia of Europa, draw the relationship

between the density of the silicate mantle and the density of the H2O layer.Comment on this curve.Question 10.3Determine the amount of heat that can be removed by convection if the ice layer

can convect. Take a viscosity of ice at its melting point equal to 1014 Pa s and anactivation energy of 60 kJ mol–1. Different viscosities at the melting point can betaken in order to investigate the effect of this parameter.

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11Astrobiology Experiments in Low Earth Orbit: Facilities,Instrumentation, and ResultsPietro Baglioni, Massimo Sabbatini, and Gerda Horneck

This chapter introduces the space environment in Earth orbit withemphasis on those parameters of outer space that are of interest toastrobiology. Facilities and scientific instrumentation to tackleastrobiological questions in Earth orbit are described. They includeexposed experiment facilities on the International Space Stationand on the retrievable satellite Foton. These facilities are also usedas examples to describe the constraints that instrument developersand experimenters have to face when developing hardware forspace missions. The chapter concludes with results obtained fromexposure experiments in Earth orbit.

11.1Low Earth Orbit Environment, a Test Bed for Astrobiology

Our biosphere has evolved for more than 3 billion years under the protectiveblanket of the Earth’s atmosphere, which shields terrestrial life against the hostileenvironment of interplanetary space. Space technology has now provided the toolsfor transporting terrestrial organic matter or organisms beyond this protectiveshield in order to study in situ their responses to selected conditions of space.It was nearly 50 years ago that the first-ever manmade object reached outer space:

the satellite Sputnik was launched by the USSR on 4 October 1957. Sputnik’s radiosignals, just simple “beeps,” were rebroadcast by television and radio stationsaround the world and immediately captured the public’s imagination. This wasthe initiation of the space age. One month later, on 3 November 1957, with SputnikII, the dog Laika became the first animal sent to space. Less than four years later,on 12 April 1961, Yuri A. Gagarin became the first human to be launched intospace, with the Soviet Vostok spacecraft, and made one elliptical orbit (181 kmperigee, 327 km apogee) of the Earth in 89 min at an inclination of 65�. At thattime, the space race between the U. S. and the USSR began, culminating in theU. S. landing of Apollo 11 on the Moon in June 1969.

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However, in the cases mentioned above, the biological systems, includinghumans, were protected from most of the hostile parameters of space, either bycontainment within a space capsule, which is a pressurized module with anefficient life support system (LSS), or at least by a space suit during extravehicularactivity. In these cases, the only space parameters of interest, or concern, weremicrogravity and radiation.Alternatively, if arriving in space without any protection, living beings are

confronted with an extremely hostile environment, characterized by a high vac-uum, an intense radiation field of solar and galactic origin, and extreme temper-atures (Table 11.1). This environment, or selected parameters of it, is the test bedfor astrobiological investigations, thereby exposing chemical or biological systemsto selected parameters of outer space or defined combinations of them.

Table 11.1 Parameters of the environment of interplanetaryspace, of low Earth orbit, and of space simulation facilities thatare relevant for astrobiological experiments.

Space parameter Interplanetary space Low Earth orbit Simulation facility

Space vacuumPressure (Pa) 10–14 10–7–10–4 10–7–10–4

Residual gas (part cm–3) 1 104–105 H104–106 He103–106 N103–107 O

Different values[a]

Solar electromagnetic radiationIrradiance (W m–2) Different values[b] 1360 Different values[c]

Spectral range (nm) Continuum Continuum Different spectra[c]

Cosmic ionizing radiationDose (Gy year–1) £ 0.1[d] 400–10 000[e] Wide range[c]

Temperature (K) > 4[b] Wide range[b] Wide range[c]

Microgravity (g) < 10–6 10–3–10–6 0–1 000

a Depending on pumping system and requirements of the experimenter.b Varying with orientation and distance to Sun.c Depending on the radiation source and filter system.d Varying with shielding, highest values at mass shielding of 0.15 g cm–2.e Varying with altitude and shielding, highest values at high altitudes and shield of 0.15 g cm–2.

Most of these studies were done in low Earth orbit (LEO), which reaches an altitudeof about 450 km. At this altitude, it takes about 90 min for a spacecraft to completean orbit around the Earth. At an inclination of 52–62�, which is that of the orbit ofthe International Space Station (ISS) – two consecutive orbits are about 2 200 kmapart (because of the progression of the Earth’s rotation). Hence, for Earth obser-vation purposes, these orbits cover most of the more inhabited areas of the globe.

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In order to understand the physical parameters imposed on astrobiological testsystems, it is first necessary to understand the space environment itself. Theenvironment in LEO is characterized by an intense radiation climate, a highvacuum, and extreme temperatures.

11.1.1Cosmic Radiation Field in LEO

Planets and moons of our Solar System are exposed to a complex radiation field ofgalactic and solar origin (Fig. 11.1). Galactic cosmic radiation (GCR) originatesoutside of our Solar System in previous cataclysmic events, such as supernovaeexplosions. When it enters our Solar System, its energies must be high enough toovercome deflection by the magnetic fields of the Solar System. Solar cosmicradiation (SCR) consists of two components, the low-energy solar wind particlesthat flow constantly from the Sun and the highly energetic solar particle events(SPE) that are emitted from magnetically disturbed regions of the Sun in sporadicbursts.The surface of the Earth is largely spared from these cosmic radiations because of

the deflecting effect of the Earth’s magnetic field and the huge shield of 1 000 g m–2

provided by the atmosphere. The terrestrial average annual effective dose equiv-alent from cosmic rays amounts to 0.30 mSv, which is about 100 times lower thanthat experienced in LEO.Sievert (Sv) is a measure of the dose equivalent, i.e., the biologically effective dose

of radiation. It is the product of a quality factor specifying the biological effective-ness of a certain radiation quality and the absorbed dose. The absorbed dose is

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Fig. 11.1 Space radiation sources of our Solar System.

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measured in Gray (Gy), with 1 Gy being equal to the net absorption of 1 J in 1 kg ofmaterial (water). In relation to the previously used unit rad, 1 Gy is equal to 100 rad.

11.1.1.1 Galactic Cosmic RadiationDetected particles of GCR consist of 98% baryons and 2% electrons. Taking thebaryonic component as 100%, then it is composed of 85% protons (hydrogennuclei), with the remainder being alpha particles (helium nuclei) (14%) andheavier nuclei (about 1%). The latter component comprises the so-called HZEparticles (particles of high charge Z and high energy), which are defined as cosmicray nuclei of charges Z >2 and of energies high enough to penetrate at least 1 mmof spacecraft or of spacesuit shielding. Though they contribute to only roughly 1%of the flux of GCR, they are considered a potential major concern to living beings inspace, especially for long-term missions at high altitudes or in high-inclinationorbits or for missions beyond the Earth’s magnetosphere. Reasons for this concernare based, on the one hand, on the inefficiency of adequate shielding and, on theother hand, on the special nature of HZE particle-produced lesions (explained inSection 11.4.3.3). The fluence of GCR is isotropic and energies up to 1020 eV maybe present. When GCR enters our Solar System, it must overcome the magneticfields carried along with the outward-flowing solar wind, the intensity of whichvaries according to the about 11-year cycle of solar activity (Fig. 11.2). Withincreasing solar activity, the interplanetary magnetic field increases, resulting ina decrease in the intensity of GCR of low energies. This modulation is effective forparticles below some GeV per nucleon. Hence the GCR fluxes vary with the solarcycle and differ by a factor of approximately five between solar minimum and solarmaximum, with a peak level during minimum solar activity and the lowest levelduring maximal solar activity.The fluxes of GCR are further modified by the Earth’s magnetic field. Only

particles of very high energy have access to low-inclination orbits. At the poles,

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Fig. 11.2 Eleven-year cycle of solar activity; the solar protonfluxes are superimposed to the sunspot numbers.

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particles of all energies can impinge in the direction of the magnetic field axes.Because of this inclination-dependent shielding, the number of particles increasesin LEO from lower to higher inclinations.

11.1.1.2 Solar Cosmic RadiationOur sun emits two types of radiation: (1) low-energy solar wind particles (mainlyprotons) that flow constantly from the sun and (2) the so-called solar particlesevents (SPEs) that originate frommagnetically disturbed regions of the sun, whichsporadically emit bursts of charged particles with high energies (Figs 11.1 and11.2). These latter events are composed primarily of protons, with a minorcomponent (5–10%) being helium nuclei (alpha particles) and an even smallerpart (1%) heavy ions and electrons. SPEs develop rapidly and generally last for nomore than a few hours; however, some proton events observed near Earthcontinued over several days. The emitted particles can reach very high energies,up to several GeV. In a worst-case scenario, doses as high as 10 Gy could bereceived within a short time, which is dangerous to both the spacecraft electronicsand the astronauts. Such strong events are very rare, typically occurring about onetime during the 11-year solar cycle. Although SPEs frequently occur during solarmaximum (Fig. 11.2), they have rarely been observed at other intervals of the solarcycle. The next solar cycle (cycle 24) will peak around the year 2010. Spacecraft inLEO are largely protected from SPEs because the Earth’s magnetic field provides alatitude-dependent shielding against SPEs. Only in high-inclination orbits doSPEs create a hazard to humans in space, especially during extravehicular activ-ities. The mechanism is the same as for GCR: particles of all energies can impinge

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Fig. 11.3 Effect of solar wind on the Earth’s magnetosphere.

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in the direction of the magnetic field axes. Hence, equatorial orbits provide thehighest radiation protection.

11.1.1.3 Radiation BeltsIn LEO, in addition to GCR and solar cosmic radiation (SCR), the radiation fieldcomprises a third source of radiation: the van Allen Belts, which result from theinteraction of GCR and SCR with the Earth’s magnetic field and with the atmos-phere. Above all, electrons and protons and some heavier ions are trapped by thegeomagnetic field in closed orbits around the Earth (Fig. 11.3). These particlesform two belts of radiation, an inner and an outer one, which differ in their type offormation. The main production process for the inner belt particles is the decay ofneutrons produced in cosmic particle interactions with the atmosphere. The outerbelt consists mainly of trapped solar particles. In each zone, the charged particlesspiral around the geomagnetic field lines and are reflected back between themagnetic poles, acting as mirrors. Electrons reach energies of up to 7 MeV andprotons up to about 200 MeV. The energy of trapped heavy ions is less than50 MeV. The trapped radiation is also modulated by the solar cycle: proton intensitydecreases with high solar activity, while electron intensity increases, and vice versa.For space missions in LEO, depending on the orbit parameters and flight data,

radiation doses in the range of 20 mSv per month may be received. Of special

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Fig. 11.4 Polar horns and South Atlantic Anomaly, regionsof elevated radiation doses in low Earth orbit at 28�, 57� and 90�inclination; numbers give doses at an altitude of 500 km behind0.2 g cm-2 aluminium shield (100 is equal to approximately860 mGy per day) (source: http://parts.jpl.nasa.gov/mmic/10.pdf).

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importance is the so-called South Atlantic Anomaly (SAA), where the fringes ofthe inner proton radiation belt reach down to altitudes of 400 km (Fig. 11.4).This behavior reflects the displacement of the axis of the geomagnetic (dipole)field by about 450 km with respect to the axis of the geoid (rotation axis), with acorresponding distortion of the magnetic field. This SAA region accounts forthe dominant fraction – up to 90% – of the total radiation exposure of spacecraftin LEO.

11.1.2Solar Extraterrestrial UV Radiation

The spectrum of solar electromagnetic radiation spans over several orders ofmagnitude, from short-wavelength X-rays to radio frequencies. At the distance ofthe Earth (1 astronomic unit = 1 AU), solar irradiance amounts to 1 360 W m–2, thesolar constant. Of this radiation, a large fraction is attributed to the infrared fraction(IR: >800 nm) and the visible fraction (VIS: 400–800 nm) and only about 8% to theultraviolet range (UV: 100–400 nm).On its way through the Earth’s atmosphere, solar electromagnetic radiation is

modified by scattering and absorption processes. Of special interest is solar UVradiation, because it has a high impact on the health of our biosphere. During thefirst 2.5 billion years of Earth’s history, UV radiation of wavelengths >200 nmreached the surface of the Earth because of lack of an effective ozone shield.Following the rapid oxidation of the Earth’s atmosphere about 2.1 billion yearsago, photochemical processes in the upper atmosphere resulted in the buildup of aUV-absorbing ozone layer in the stratosphere. Today, the stratospheric ozone layereffectively absorbs UV radiation at wavelengths shorter than 290 nm (Fig. 11.5).

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Fig. 11.5 Spectrum of solar UV radiation: extraterrestrial, at thesurface of the early Earth (the first 2.5 billion years), at the surfaceof the present Earth, and spectral UV sensitivity of the geneticmaterial DNA.

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The spectrum of extraterrestrial solar UV radiation has been measured duringseveral space missions, such as Spacelab 1 and the European Retrievable Carrier(EURECA) mission. It can be divided into three spectral ranges: UV–C(200–280 nm), contributing 0.5%; UV-B (280–315 nm), contributing 1.5%; andUV-A (315–400 nm), contributing 6.3% to the whole solar electromagnetic spec-trum. UV radiation of wavelengths shorter than 200 nm, which is absorbed by themolecules of the atmosphere, belongs to the vacuum UV. Although the UV–C andUV-B regions make up only 2% of the entire solar irradiance prior to attenuationby the atmosphere, they are mainly responsible for the high lethality of extrater-restrial solar radiation to living organisms (see Section 11.4). The reason forextraterrestrial solar UV radiation’s high lethality – compared to conditions onEarth – lies in the absorption characteristics of DNA, which is the decisive target forinactivation and mutation induction by UV (Fig. 11.5). Its absorption maximumlies in the UV–C range. If photons of this UV range are absorbed, they induce avariety of photochemical reactions of the nucleic acid bases, such as dimerizationof adjacent pyrimidine bases. If not properly repaired, these photoproducts in theDNA lead to mutation or even inactivation of the cells.

11.1.3Space Vacuum

In free interplanetary space, pressures down to 10–14 Pa prevail. Within the vicinityof a body in space, the pressure may significantly increase due to outgassing. InLEO, pressure reaches 10–6 to 10–4 Pa. The major constituents of this environmentare molecular oxygen and nitrogen as well as highly reactive oxygen and nitrogenatoms. In the vicinity of a spacecraft, the pressure further increases, depending onthe degree of outgassing. For example, in the Shuttle cargo bay, a pressure of3 · 10–5 Pa was measured.If the pressure reaches values below the vapor pressure of a certain material, the

material’s surface atoms or molecules vaporize. Dehydration is the main processaffecting biological samples in outer space. In addition to moisture, sealants,lubricants, and adhesives are the main substances that outgas from spacecraft.However, even metals and glasses can release gases from cracks and impurities.These gas products may condense again onto optical elements, thermal radiators,or solar cells, thereby obscuring them.

11.1.4Temperature Extremes

In space, the temperature of a body, which is determined by the absorption andemission of energy, depends on its position with respect to the Sun and otherorbiting bodies, as well as on its surface, size, mass, and albedo (reflectivity). InLEO, the energy sources include solar radiation (1 360 W m–2), the Earth albedo(480 W m–2), and terrestrial radiation (230 W m–2). Periodically, an orbiting objectcan be shaded from the sun as it passes on the Earth’s night side. Within an orbit

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lasting 90 min, the spacecraft is exposed to the sun for about 60 min and movesinto the Earth’s shadow for the residual 30 min. Therefore, in LEO, the temper-ature of a body can reach both extremely high and extremely low values within90 min. For the International Space Station (ISS), tolerable temperature limits aredefined as +120 �C being the highest value and –120�C being the lowest.There are at least five elements that influence the temperature a biological

sample experiences in space:• inclination of the orbit,• experiment view angle relative to the Sun,• absence of convection resulting from microgravity condi-

tions,• extent of conduction, which is influenced by the thermal link

between experiment and spacecraft interface, and• extent of radiation, which is influenced by the vicinity to other

payloads on the spacecraft.

11.1.5Microgravity

Because of the presence of masses in our Universe, true zero gravity does notexist, and even within the ISS at an altitude of 350 km, the level of gravity is onlyabout 8% less than the gravitational field at the Earth’s surface. In order toachieve a condition of reduced gravity, the spacecraft has to be accelerated so thatthe gravitational force and the centrifugal force are equal in amount but withopposite vectors. Actually, the spacecraft is in a state of freefall. The resultingacceleration condition is called “microgravity,” because a residual acceleration inthe range of 10–4 to 10–6 g cannot be excluded. Compared to the “gravity environ-ment” on Earth, various physical phenomena behave differently in the theoreticalstate of zero acceleration. Sedimentation, hydrostatic pressure, and convection arelinearly proportional to gravity and therefore become zero in weightlessness;however, diffusion still persists in microgravity. Several experimental and tech-nical designs have been developed to study the effect of acceleration on thephysiology of living systems and thus identify potential problems during long-term space flight.

11.2Astrobiology Questions Tackled by Experiments in Earth Orbit

Space technology has opened a new opportunity for life sciences by providing thevehicle to transport terrestrial organic matter or organisms beyond the protectiveblanket of our atmosphere in order to study in situ their responses to selectedconditions of space. Since the 1980 s, with the accessibility of Spacelab, the free-flying satellite European Retrievable Carrier (EURECA), and the Russian Cosmos andFoton satellites, the European Space Agency (ESA) has provided opportunities for

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experiments in Earth orbit. By utilizing outer space or special components of thisenvironment as a tool, specific questions of astrobiology were tackled. Thesestudies include but are not limited to:

• the understanding of the relevance of extraterrestrial organicmolecules to the delivery of the building blocks of life onEarth or on any other planet;

• the understanding of the role of solar extraterrestrial UVradiation and cosmic radiation in the evolution of potentialprecursors of life in space;

• the reproduction of processes dealing with the prebiotic andbiological evolution on Earth or any other celestial body ofastrobiological interest;

• the likelihood of interplanetary transfer and the limitingfactors of panspermia, the hypothesis of the distribution oflife beyond its planet of origin;

• the simulation of the UV radiation climates of the early Earthor present Mars in order to assess their habitability;

• estimations on the upper boundary of the biosphere; and• concepts of suprathermal reactions in space.

11.3Exposure Facilities for Astrobiology Experiments

Following increasing requests from the scientific community to acquire data on theeffects of the space environment on biological and material/component samples,the ESA promoted in the early 1990s the development of BIOPAN, a multi-usermulti-mission facility conceived for space exposure recoverable experiments ofshort durations (two weeks). Provided with its own heat shield, a hinged motor-driven lid, and a package of scientific sensors, it has been flown six times already,experiencing only one mishap in 2002 with the Foton M1 launch accident. It has avery good record of completed experiments, and a valuable amount of data hasbeen collected so far. One more flight is currently planned in 2007 with Foton M3.Another multi-user exposure facility, EXPOSE, is being developed at the time of

this writing (2006). It is designed for the outer platforms of the International SpaceStation (ISS) and supports long-duration experiments (one to three years). Twoattachment points are foreseen for EXPOSE:

• one of the external platforms of the European Columbusmodule as part of the European Technology Facility (EUTEF)and

• the URM-D platform, an external ISS facility at the RussianZvezda module.

A more intensive utilization of these facilities is envisaged in the future in supportof the new ESA Exploration Program.

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11.3.1BIOPAN

BIOPAN is based on the heritage of a low-tech Russian exposure container calledKNA (Kont�jner Nafflchnoj Apparatfflry: Container of Scientific Equipment). KNA,used by the ESA for radiobiological experiments on three Russian BION missionsin 1987, 1989, and 1992, was a passive experiment container with a hinged lid. Thelid was open during launch – with the experiments protected only by the nosefairing of the launcher – and during orbital flight. Before landing, the spring-loaded lid was closed so that the experiments were safely stored during reentry.The lessons the ESA learned from KNA directly resulted in the concept of

BIOPAN. Although some basic characteristics of KNA were maintained (a pan-shaped structure, a movable lid, experiment positions in the bottom part and in thelid), BIOPAN is much more advanced in terms of versatility, controllability, size,experiment accommodation, and data acquisition. In BIOPAN, the lid is openedand closed by telecommand, housekeeping status data are down-linked during theflight, the space environment is monitored by a set of integrated sensors, andunwanted temperature excursions in orbit can be countered by active means(heaters), by passive means (insulation blankets), or by closing the lid.BIOPAN hosts exobiology, radiobiology, and materials science experiments,

aimed at evaluating the combined or individual effects of solar UV light, spaceradiation, vacuum, extreme temperatures, and microgravity on biological samples,materials specimens, and electronic components.After a successful test flight in 1992, BIOPAN completed four operational

missions in• 1994 (Foton 9),• 1997 (Foton 11),• 1999 (Foton 12), and• 2005 (Foton M2).

In 2002 a flight unit (flying as BIOPAN-4) was lost in the Soyuz launch failure ofFoton M1. A seventh flight with an upgraded version of BIOPAN is scheduled forlate 2007, onboard the Russian Foton M3 satellite.

11.3.1.1 Technical Characteristics of BIOPANBIOPAN is a 27-kg experiment container, designed to fly with Russian spacecraftof the Foton class (Fig. 11.6). The first Foton was successfully flown in 1985. Thesatellite, typically launched with a Soyuz U vector, consists of three modules:

• the descent module,• the battery pack, and• the attitude control module.

The descent module is a pressurized spherical capsule where most of the scientificpayloads are accommodated. Foton is capable of carrying up to 600 kg of scientific

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payload, with an average daily power budget available to the scientific payloads of400 W (on a typical two-week mission). The residual acceleration levels onboard arebetween 10–4 g and 10–6 g. Protected by a heat shield, the pressurized sphericalcapsule is the only part of the satellite returning to Earth at the end of the mission.The payload is then retrieved and returned to the investigators within two days afterlanding.BIOPAN is mounted onto the external surface of the descent module (Fig. 11.7),

protruding from the thermal blanket, which is wrapped around the satellite shortlybefore launch. Power and data links are provided via cables whose connectors arestrapped away at the separation of the satellite modules during atmosphericreentry. An internal battery provides energy to BIOPAN subsystems from thereentry phase onwards.The upper shell of the container is a motor-driven lid, which, once in orbit

(typically a few hours after liftoff, depending on the experiment requirements),

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Fig. 11.6 Foton 12 spacecraft carried to theSoyuz launcher, in the MIK integration facility atPlesetsk Cosmodrome (Russia) in September1999 (photo credit: ESA).

Fig. 11.7 Installation of BIOPAN onto thedescent module of the satellite Foton, duringthe pre-launch operations (photo credit: ESA).

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turns open at 180 �, allowing the experiment samples be exposed to the spaceenvironment (Fig. 11.8).At the end of the mission the lid is closed again by telecommand sent from

ground, although a pre-programmed internal backup command ensures the prop-er execution in case of communication problems. In nominal operations, the lidremains open throughout the entire mission and is closed just before reentry of thecapsule. To withstand the extreme heat during reentry, the entire BIOPAN struc-ture is protected by an ablative heat shield of the same kind used for the capsuleitself. For the safety of the facility and its closing device, the closure of the lid alsomay occur in orbit in case of temperatures exceeding the nominal range.BIOPAN is provided with a variety of sensors to monitor and record the

environmental history of the mission. Included are a UV sensor, a radiometer,an active radiation dosimeter, and a set of eight thermistors to measure theexperiment temperatures at different locations. The sensor data are stored onboardduring flight. Electrical heaters and experiment-customized thermal blankets(multilayer insulators) are used to keep the biological specimen within pre-deter-mined temperature ranges and to provide minimum shielding against soft cosmicradiation.

11.3.1.2 Experiment Hardware Accommodated within BIOPANThe experiment packages – up to a total mass of 4 kg, a maximum height of50 mm, and a total available surface area of 1 100 cm2 – can be individuallydesigned by the investigators. They are installed on two mounting plates, one inthe bottom part and one in the lid (Fig. 11.8). The research covers differentscientific and technical fields, from astrobiology (see Section 11.4) and materialsscience to components tests and validation. In Tables 11.2 to 11.4, experiments arelisted that so far have been flown on BIOPAN/Foton missions.

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Fig. 11.8 Configuration of BIOPAN. Drawing (a) and photo (b)of BIOPAN fully open with the experiment hardware integrated,before flight (courtesy of ESA).

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Table 11.2 Foton/BIOPAN missions since 1992.

Mission Year Payload

Foton-8/ BIOPAN-0 1992 Test flight with non-ESA-sponsored experimentsFoton-9/ BIOPAN-1 1994 6 experiments: Base, Shrimp, Mapping, Survival, Vitamin,

DustFoton-10 1995Foton-11/ BIOPAN-2 1997 6 experiments: Base, Shrimp, Mapping, Survival, Vitamin,

DustFoton-12/ BIOPAN-3 1999 4 experiments: Survival, Yeast, Dosimap, VitaminFoton-M1/ BIOPAN-4 2002 9 experiments – lost (launch failure)Foton-M2/ BIOPAN-5 2005 9 experiments: Marstox, Letvar, Photo I, Rado, Lichens,

Organics, Yeast II, R3D-B, PermafrostIn preparation:Foton-M3/ BIOPAN-6 2007 10 experiments: R3D-B2, UV-olution, Highrad, Yeast III,

Life, LMC, Tardi A & B, Lithopanspermia,Marstox II, Rado II

Table 11.3 Experiments flown in BIOPAN in the period 1992–1999.

Research topic Principle investigator

Radiation dosimetryRadiation measurements behind defined shieldings G. Reitz, DLR, CologneDepth dosimetry L. Adams, ESTEC, NoordwijkDepth dosimetry Yu. Akatov, RCSRS, MoscowNeutron dosimetry V. Dudkin, RCSRS, MoscowUV dosimetry V. Tsetlin, IBMP, MoscowHZE and LET measurements A. Vikhrov, RCSRS, MoscowHZE and LET measurements E. Benton, USA

Radiation biologyRadiation damage in plant seed DNA bases in situ J. Cadet, CEA, GrenobleRadiation damage in embryos of the brine shrimp A. Hernandorena, CERS, BiarritzEffects of soft radiation in yeast cells J. Kiefer, University of GiessenEfficiency of radioprotecting drugs J-P. Moatti and N. Dousset, Un. P. Sabatier

AstrobiologyEffects of solar UV on peptides in artificialdust grains

A. Brack, CNRS, Orl�ans

Survival rate of biological organisms G. Horneck, DLR, Cologne

Materials and components validationBit flips in EEPROM cards exposed to spaceradiation

R. Harboe Sørensen, ESTEC

Stability of coating materials outside exposedin space

M. van Eesbeek, ESTEC

Stability of thermal-control coating materialsexposed in space

E. Overbosch, Fokker Space, Leiden

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Table 11.4 Experiments flown in BIOPAN 4 and 5(2002 and 2005).

Experiment Principal investigator

Marstox (D) P. Rettberg and G. Horneck, DLRYeast II (D) J. Kiefer and M. Loebrich, Saarland UniversityPhoto I (I) M.T. Giardi, CNR RomeOrganics (NL) P. Ehrenfreund, Leiden UniversityR3D-B (D) D. Haeder, Erlangen UniversityLichens (E) L. Sancho, Madrid UniversityLetvar (D, A) N. Vana, Wien UniversityPermafrost (Ru) D. Gilichinsky, RASRado (Ru, Hu) V. Shurshakov and J. Palfalvi, IBMP

The experiment temperature profile in orbit is selectable: either a non-controlledmode with temperatures freely oscillating between £ –35�C and ‡ +10 �C, in syn-chrony with the alternating periods of solar illumination and shadowing; or acontrolled, stable temperature with a fixed set point in the range of 10–25 �C usingheaters and dedicated thermal insulators.The experiments flown in the past five BIOPAN missions have been accommo-

dated in sample holders specifically designed by the scientific teams under ESAsupervision. In addition to complying with the carrier interfaces, they are requiredto pass a number of qualification tests, which include a vibration test according tothe Foton specification levels and a thermocycling test performed in a thermo-vacuum chamber.The typical experiment environment offered by BIOPAN includes:

• a microgravity level of <10–5 g;• a radiation level up to 6 Gy (600 rad) per day and up to 80 Gy

(8 000 rad) per 15-day mission (depending on solar activityand shielding; see Section 11.1);

• solar electromagnetic radiation on the order of 40 solarconstant hours per mission, and

• the possibility of controlled temperature profiles at thoseexperiment packages that are thermally decoupled from eachother.

At flight completion, when BIOPAN is carried back from the landing site to theESA ESTEC clean room and opened in a controlled environment, these packagesare dismounted, inspected, and returned to the investigators, who examine theircontents in their own laboratories around Europe. Reference samples are storedin BIOPAN under identical conditions but shielded against UV. Additionalcontrol samples are maintained on the ground under controlled terrestrial con-ditions.

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11.3.1.3 Operational Aspects of BIOPANThe typical operational cycle of BIOPAN includes satellite interface tests threemonths prior to launch (L), experiment integration at L – 1 week, two weeks oforbital flight, and return of the experiments to the investigators four days afterlanding. The main figures of a typical Foton-BIOPAN mission are shown in Table11.5. Parameters such as flight duration, altitude, and energy available for thepayload can be modified depending on the chosen mission profile and on theupgrading of the satellite (e.g., for the Foton M version).

Table 11.5 Main figures of a typical BIOPAN mission onboarda Foton satellite.

Flight parameter Flight data

Flight frequency Once every two yearsBIOPAN’s models 1–3Flight duration 14–16 daysAltitude 220–390 kmInclination 62.8 �Energy available (15 days) 3 kWh (164 Ah )

Integration of BIOPAN and interface testing with Foton take place approximatelythree months before the launch at the Foton construction site in Russia. At thisstage, the manufacturing of the satellite and of its subsystems is completed, and allthe necessary electrical and mechanical interface tests between carrier and pay-loads need to be carried out. The BIOPAN flight unit performances and itsinterfaces with Foton are verified through a sequence of mechanical and electricaltests. Dedicated electronic ground support equipment is used to support theseactivities.During these tests, the satellite undergoes a simulated mission profile in which

all the various commands are issued and each subsystem is checked. These testsare meant to qualify the satellite for the mission, to control the readiness of eachpayload, and to verify possible mutual interference between the carrier and scien-tific instruments. After successful completion of these tests, BIOPAN is dis-mounted, packed, and transported back to ESTEC. This operation is necessary toallow the integration of the biological samples at a very late stage at ESTEC, asdemanded by the nature of these experiments. In contrast, most of the otherscientific payloads remain inside Foton and are transported with the satellite tothe launch site (Plesetsk Cosmodrome or Baikonour Cosmodrome).The sensitivity of the biological samples – often including yeast cells, spores,

bacteria, and plants seeds – to storage effects such as temperature variation,humidity, and/or aging requires their preparation in well-controlled environmen-tal conditions shortly prior to launch. They are prepared in the investigators’laboratories up to 10 days in advance and delivered to ESA-ESTEC in thermally

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controlled containers. They are integrated into BIOPAN one week before launch.This solution is preferred to an integration “onsite” at Plesetsk or Baikonourbecause of the lack of dedicated equipment and suitable laboratories there.At L – 4 days, an ESA team carries the BIOPAN flight unit with the samples from

ESA-ESTEC to the launch site, using a special Russian charter plane. Contained ina special battery-powered thermal container until the last minute, BIOPAN isfinally installed onto the capsule at L – 3 days, a few hours before the final closingof the Foton hatches.The spacecraft is then ready to be integrated with the launcher. Charged with its

complete payload complement, and a mass of 6.5 tons, Foton is lifted from itssupporting stand, lowered into the fairing coupling ring, and closed within the twohalf shells of the Soyuz nosecone (Fig. 11.9). In this configuration, it is then tiltedhorizontally and coupled to the third stage of the rocket, before being lifted up andlaunched.Once in orbit, the telecommand to open the lid of BIOPAN is issued from the

ground at a time that can be decided based upon the experiment needs (typicallybetween 10 min and 20 h after liftoff).In orbit, the position and the status of the Foton satellite and of BIOPAN are

monitored via telemetry. The telemetry data include the main parameters, repre-sentative of the BIOPAN status (position of the lid, power and energy budgets),while the other housekeeping and scientific data from the sensors are storedonboard and analyzed after the mission (Fig. 11.10). The lid closure is againcommanded from the ground approximately one day before landing.After completion of the mission, the Foton satellite is de-orbited when its ground

track is favorable for a landing within the Russian territory or in Kazakhstan.

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Fig. 11.9 Final assembly of Foton with theSoyuz nosecone. BIOPAN is visible on the topof the descent module (photo credit: ESA).

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The capsule reentry is assisted with a parachute system and a retro-rocket thatdecrease the landing shock down to values on the order of 35–40 g. This system isactivated just a couple of meters before the final touchdown, via a gamma-raysource installed in the heat shield. Every payload, including BIOPAN, has to be

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Fig. 11.10 Environmental data recorded during the BIOPAN-3/Foton 12 mission. Top: Time profile of the radiation exposuremeasured by radiometer and UV meter. Bottom: Temperaturedata recorded in the lid of BIOPAN for the experiments withouttemperature control (courtesy of ESA).

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designed to withstand a possible landing shock of 90 g (duration: 40–50 ms), whichmight occur in the case of retro-rocket malfunctioning.After separation of the descent module from the battery pack (some 30 min

before final landing), themain power is cut off from the instruments, which meansthat thermal control is no longer assured. Rescue teams reach the landing site withhelicopters from the closest military base.A prompt finding of the satellite in the Russian-Kazakh steppes (not always easy,

especially with unfavorable weather conditions) and an early recovery of the experi-ments is fundamental for the mission success of BIOPAN (Fig. 11.11). BIOPAN isthen dismounted from the burnt satellite heat shield and, still closed and locked,placed in its cooled transport container and carried back to Samara. Here, themission data are downloaded and the payload is then transported back to ESA-ESTEC the day after. The opening of BIOPAN and experiment de-integration anddelivery to the investigators are performed in an ESA-ESTEC clean room withinfour days after landing.

11.3.1.4 Orbital Characteristics of a BIOPAN MissionThe orbital parameters selected for Foton, the carrier spacecraft of BIOPAN, havenot noticeably changed since its first flight in 1992 (Table 11.6). With the intro-duction of Foton-M in 2002, the orbital trajectory became slightly more circular inorder to optimize the microgravity levels. From Foton-M2 onwards, a differentlaunch site is used (Baikonur rather than Plesetsk), but this has almost no effect onthe orbital inclination. The consistency of the orbital parameters enables theBIOPAN investigators to repeat their experiments if necessary under conditionsthat – apart from the sun cycle events – are remarkably similar. It also means thatthe experiment environment for upcoming flights may largely be predicted fromthe recordings made during previous missions.

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Fig. 11.11 Foton descent module with BIOPANat the landing site (photo credit: ESA).

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Table 11.6 Orbital parameters, flight duration, and launch siteof the BIOPAN missions.

Mission Spacecraft Apogee Perigee Inclination Duration Launch site

BIOPAN-0 Foton-8 383 228 62.8 � 15.6 d PlesetskBIOPAN-1 Foton-9 385 227 62.8 � 17.6 d PlesetskBIOPAN-2 Foton-11 385 227 62.8 � 13.6 d PlesetskBIOPAN-3 Foton-12 405 225 62.8 � 14.6 d PlesetskBIOPAN-4[a] Foton-M1 304 262 62.8 � 15.6 d PlesetskBIOPAN-5 Foton-M2 304 262 63� 16 d BaikonurBIOPAN-6 Foton-M3 304 262 63� 13 d Baikonur

a Orbital parameters and flight duration of BIOPAN-4 as announced before the crash.

11.3.1.5 Environment of BIOPAN ExperimentsTemperature, pressure, and solar irradiation at the experiment site are monitoredby an integrated set of BIOPAN sensors. The data are stored onboard during themission and can be accessed after the flight. Irradiation by cosmic rays is moni-tored by investigator-provided detectors. The microgravity environment is notmeasured inside BIOPAN itself but inside the Foton capsule by ESA-providedsensors.The temperature history of the experiment samples in orbit depends on the

amount of thermal insulation (single foils or multilayer blankets), the thermalcoupling to the BIOPAN carrier plates, and the use of heaters. It was observed thata non-insulated experiment decoupled from an unheated carrier plate may expe-rience extreme temperature fluctuations from –40 �C to +60�C. In contrast, aninsulated experiment that is tightly coupled to a heated carrier plate can bemaintained at a stable temperature, selectable between +15 �C and +25�C(Fig. 11.10).The possibility of overheating during atmospheric reentry at the end of the

mission was recognized early during the development of BIOPAN. Therefore, aquite massive heat shield was designed for BIOPAN. While the total weight ofBIOPAN is close to 27 kg, including the experiments, the heat shield is responsiblefor 12 kg of that figure. As a result, the peak temperatures during reentry and afterlanding recorded inside BIOPAN never exceeded +30�C.BIOPAN is also equipped with a pressure sensor for rough monitoring of gas

release from BIOPAN (evacuation) during ascent.Irradiation by solar light (including UV radiation) is measured by two types of

sensors. A radiometer monitors the input of solar electromagnetic radiation overthe entire spectrum from UV to IR. Special UV sensors are added to monitor thesolar wavelength ranges that are specific to orbital flight. (At the surface of theEarth, there is no incidence of solar UV–C and only a limited incidence of UV-B;see Fig. 11.5.) On the four missions completed so far, the total dose of sunlight hasvaried from 8.2 kJ cm–2 to 20.4 kJ cm–2 (Table 11.7). The total dose largely de-

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pended on the time when the lid of BIOPAN was open in orbit. This period variedfrom 7.8 to 14.8 days (Table 11.7). As a consequence, the daily dose varied from0.99 kJ cm–2 to 1.38 kJ cm–2, which corresponds to solar constant hours of2.02–2.80. On the four missions completed so far, the total dose of specific energyderiving from solar electromagnetic radiation varied from 8.2 kJ cm–2 to20.4 kJ cm–2. Some BIOPAN flights performed measurements of UV–C, UV-B,and UV-A radiation in addition to the solar radiation sensors that integrate over thewhole solar spectrum.

Table 11.7 Data of solar irradiation during different BIOPANmissions.

Mission Lid open Total dose Daily dose

BIOPAN-0 187 h = 7.8 d 8.2 kJ cm–2 1.05 kJ cm–2 2.14 SCh[a]

BIOPAN-1 355 h = 14.8 d 20.4 kJ cm–2 1.38 kJ cm–2 2.80 SChBIOPAN-2 239 h = 9.9 d 12.9 kJ cm–2 1.30 kJ cm–2 2.65 SChBIOPAN-3 302 h = 12.6 d 12.5 kJ cm–2 0.99 kJ cm–2 2.02 SCh

a SCh = solar constant hours.

The dose received from cosmic radiation is measured in different radiation dosim-etry experiments of BIOPAN. Depending on the level of shielding, the experimentsin BIOPAN may absorb a radiation dose up to 5.6 Gy per day, which is four ordersof magnitude higher than the daily dose received inside the Foton capsule or insidethe ISS. However, the actual radiation dose absorbed by the experiment samples inBIOPAN is generally much smaller than this value because of their containment. Asmall change in shielding density may create a dramatic difference. Over the first0.05 g cm–2 of shielding mass, the radiation dose falls steeply down by one order ofmagnitude, over the first 0.25 g cm–2 by two orders of magnitude, and over the first1 g cm–2 by three orders of magnitude.The microgravity environment was measured by ESA on Foton-12, the spacecraft

that carried BIOPAN-3. The quasi-steady acceleration level was below 10–4 g over allthree orthogonal axes.

11.3.2STONE

The STONE experiments aim to study the physical, chemical, and biologicalmodifications caused by atmospheric entry in rocks, in meteoritic materials, andin their possible embedded organisms. For this purpose, different types of rock,loaded with microorganisms, are mounted in the heat shield of the Foton reentrycapsule. During reentry into the atmosphere at the end of the two-week flight, theSTONE rock samples are subjected to temperature and pressure loads comparableto those experienced by meteorites.

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The rationale for the STONE experiments is as follows (see also Chapter 1): mostof the 25 000 known meteorites originate from the asteroid belt. There are 18meteorites that definitely come from the Moon; most are regolith samples, aswould be expected when rocks are propelled from planetary surfaces by impact.Then there are the 37 so-called SNC meteorites, which are quite distinct fromasteroidal debris and which come fromMars (see Chapter 8), but none of them is asurface sample. Because Mars once had a warm and wet climate, its surface mustbe covered by both impact-generated regolith and sedimentary rocks deposited byrunning and/or still water. The sedimentary rocks should comprise detrital depos-its as well as chemical sediments such as evaporites. In addition, groundwater cancompact loose sediments and regolith by filling the pore spaces with evaporiticminerals. Such consolidated sedimentary hard rocks should be among the Martianmeteorites, but they are not. It is possible that they survived their traumatic escapefrom Mars but not their terrestrial atmospheric entry because of decrepitation inthe cementing mineral (very likely to be a sulfate). Therefore, STONE investigatedwhether such rocks would be destroyed or damaged by atmospheric infall,although Foton’s reentry speed of 7.8 km s–1 is considerably lower than thatexperienced by a meteorite (20–70 km s–1).The STONE experiments take advantage of the accommodation on the heat

shield of the reentry capsules of the Russian retrievable carriers of the Foton class.They are normally placed around the descent module’s hottest point (stagnationpoint), inserted into the heat shield with specially designed holders that are madeof the same ablative material used for the heat shield (Fig. 11.12). Because the rocksample’s thermal conductivity is generally of some order of magnitude higher thanthat of the capsule shielding, a protective layer is placed underneath the exposedsample, between the metallic structure of the capsule and the rock sample itself.STONE-1 was conducted in 1999 on Foton-12. Three different types of rock were

fixed into the ablative heat shield of the Foton reentry capsule:• a basalt,• a dolomite (sedimentary rock), and• a simulated Martian regolith sample.

The goal was to investigate why all Martian meteorites so far collected on Earthwere exclusively of the igneous type, while the surface of Mars consists, apart fromigneous rocks, largely of sedimentary materials. The experiment provided a pos-

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Fig. 11.12 STONE-5 samples installed onto theFoton M2 heat shield. Picture taken before themating of the descent capsule with the attitudecontrol module (photo credit: ESA).

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sible explanation for this dilemma: it showed that a sedimentary rock (the dolo-mite) can survive the atmospheric entry process, but after landing, it will easilydecompose from the chemical and physical changes it has suffered.Follow-on experiments were prepared in 2000 (STONE-2), 2001 (STONE-3), and

2002 (STONE-4), but unfortunately none was completed. STONE-2 failed becauseits carrier was heavily damaged during reentry and touchdown, whereby the rockswere lost. STONE-3 was never launched because of programmatic changes.STONE-4 was carried by the Foton-M1 capsule, which was lost when the launcherrocket crashed shortly after liftoff.The STONE-5 experiment was partly a repetition of STONE-1. A sandstone

(a sedimentary rock) and, for comparison, a dolerite (an igneous rock) wereexposed to the reentry environment. A new aspect of this experiment is theemphasis on biology: both rocks were loaded with microorganisms. This allowedthe scientists to investigate the chances for survival of simple life forms transportedby meteorites when entering the atmosphere of the Earth. The third rock fromSTONE-5 was a gneiss (a metamorphic stone) from Antarctica carrying endolithiccyanobacteria (desiccated, vegetative cells).

11.3.3EXPOSE

The EXPOSE facility, conceived to support astrobiology and radiation biologyresearch in space, was designed and developed by ESA to fly on the externalplatforms of the ISS, originally on the Columbus external balconies. EXPOSEwill host experiments prepared by scientists from various European researchinstitutes. Experiment specimens will be located in hundreds of tiny cells, pres-surized or vented, protected with windows and filters of various geometries andmaterials. Most of the selected experiments deal with understanding the influenceof the radiation environment, in all its different components, on selected biologicalsamples and organic compounds. Some of them are part of a research programthat includes among its targets the understanding of organic matter’s survivabilityof extraterrestrial conditions, such as on Mars.The EXPOSE development started in 2001. After undergoing a full qualification

program, in 2004 the Flight Model passed its flight acceptance review and wasdelivered to Columbus for integration (EXPOSE-E). Because of delays in the launchof Columbus, ESA investigated in 2004 the possibility of flying EXPOSE on theRussian segment of the ISS (RS-ISS), mounted on a recently installed externalplatform (named URM-D), in order to provide European scientists with an earlierand strongly demanded flight opportunity (EXPOSE-R).

11.3.3.1 EXPOSE FacilityThe EXPOSE facility includes three experiment trays (Fig. 11.13), each one con-taining four sample carriers; some of them are sealed and allow accommodation ofpressurized containers, while others are vented via a venting system integrated in

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the tray. The air channel is sealed with a dedicated valve, which opens after thefacility is brought out to the external surface of the ISS by a dedicated controlcommand.Each sample carrier is structured in two or three layers (for sample exposure to

solar radiation and for dark control) and accommodates a variety of sample cells ofdifferent size and geometry (from 16 to 64 per layer), each one equipped withdifferent kinds of optical windows, filters, and dosimeters. All biological samples,such as bacterial cells or spores, fungal spores, fern spores, or plant seeds, aredeposited in dry layers on quartz or MgF2 disks. Pressure integrity is provided bymeans of a rubber gasket between the metallic tray housing and the glass.The EXPOSE experiments are designed for one to two years’ external exposure to

outer space. According to the EXPOSE experiment procedure, preparation of thebiological samples, deposition on quartz glasses, drying and accommodation in thecarriers, placement of the carriers in the trays, and final assembly of the EXPOSEfacility will be carried out at ground laboratories.In addition to the trays, the facility accommodates various sensors that measure

parameters characterizing the experiment conditions (solar radiation, temperature,etc.) and an electronic unit that acquires, formats, and transfers these data to theISS service systems.The EXPOSE assembly includes the EXPOSE facility and its supporting struc-

ture, interfacing with the EUTEF-CEPA (Columbus External Platform Adapter) for

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Fig. 11.13 EXPOSE facility, the external facility of the ISS.(A) Photo of EXPOSE-E; (B) drawing of EXPOSE assembly(courtesy of ESA).

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EXPOSE-E or with the external platform (named URM-D) of the RS-ISS forEXPOSE-R.The EXPOSE-E facility provides common functionalities and services and a

controlled environment to the experiment samples (shutters, scientific and house-keeping data acquisition and transmission, thermal control). It includes the follow-ing subsystems:

• structure and mechanisms;• shutters (including lids, hinges, shutter drives);• trays (including windows, seals, valves, connectors);• sample carriers (including windows, filters, controls);• EXPOSE control unit (motor and valves control, data

acquisition);• sensors (temperature, pressure, UV, proximity); four sensor

packages (UV-B and radiometer) are positioned on the fourfacility corners;

• a thermal control system, based on heaters, multilayer insu-lators (MLI), and coatings;

• an electrical interface (I/F) to EUTEF Data Handling andPower Unit; and

• a mechanical I/F to EUTEF-CEPA (I/F bracket).

The EXPOSE actuators are controlled by software via the experiment control unitmicro-controller; they can also be operated via the telemetry/telecommands(TM/TC) link. In particular, the micro-controller provides the following functions:

• acquisition and transmission of housekeeping data and datafrom eight temperature and five solar sensors;

• acquisition and transmission of R3D data;• data storage (in case of data link interruption);• command and control of three motor-driven lids (shutters) by

stepper motors;• command and control of three motor-driven valves for vented

experiment compartments;• thermal control of experiments achieved with two different

sets of heaters, thermostat controlled, positioned underneatheach experiment tray and on the inner side of the facilityframe; and

• overheat protection via automatic lid closure whenever apredefined temperature is exceeded.

11.3.3.2 EXPOSE ExperimentsThe experiments selected for the flight of EXPOSE-R are listed in Table 11.8. Theexperiments selected for the flight of EXPOSE-E with Columbus are listed inTable 11.9.

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Table 11.8 Experiments selected for EXPOSE-R.

Principal investigator Experiment Topic of research

C. CockellOpen University (UK)

ROSE-1/ENDO To assess the impact of extraterrestrialUV radiation on microbial primary pro-ducers (algae, cyanobacteria)

R. Mancinelli SETI Institute,NASA Ames (USA)

ROSE-2/OSMO To assess the protective effects on osmo-philic microorganisms enclosed withingypsum-halite crusts

G. Horneck DLR (D) ROSE-3/SPORES To assess the protection of spores by me-teorite material against space conditions:UV, vacuum, and ionizing radiation

J. Cadet C.E. N. G. (F) ROSE-4/PHOTO To determine the photoproducts result-ing from exposure of dry DNA samples orbacterial spores to solar UV radiation

N. Munakata Universityof Tokyo, Japan

ROSE-5/SUBTIL To determine the mutational spectra ofBacillus subtilis spores induced by spacevacuum and/or solar UV radiation

G. Ront� Research Lab. forBiophysics, Budapest (HUN)

ROSE-8/PUR To determine the biologically effectivedose of solar extraterrestrial UV radiationby biological dosimetry

A. Brack CNRS- Orleans (F) AMINO To study photochemical processing ofamino acids in Earth orbit

P. Ehrenfreund LeidenObservatory (NL)

ORGANICS To study the evolution of organic matterin space

D-P. H�der Universityof Erlangen (D)

R3D Radiation dosimetry

Table 11.9 Experiments selected for EXPOSE-E.

Principal investigator Experiment Topic of research

G. Horneck DLR (D) PROTECT To determine the resistance of spacecraftisolates to outer space for planetary pro-tection purposes

D. Tepfer CNRS, Versailles (F) SEEDS To test plant seeds as a terrestrial modelfor a panspermia vehicle and as a sourceof universal UV screens

H. Cottin University 5, Paris PROCESS To study prebiotic organic chemistry onthe ISS

P. Rettberg DLR (D) ADAPT To study molecular adaptation strategiesof microorganisms to different space andplanetary UV climate conditions

S. Onofri Universita’deglistudi della Tuscia di Viterbo (I)

LIFE To study the resistance of lichens andlithic fungi in space conditions

D-P. H�der Universityof Erlangen (D)

R3D-2 Radiation dosimetry

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11.3.3.3 EXPOSE Experiment HardwareThe experiments of EXPOSE (Tables 11.8 and 11.9) are accommodated in threeexperiment trays. They are equipped with four squared recesses, 77 · 77 · 26 mmeach, where the sample carriers are inserted. These are lightweight elementshousing a number of sample cells whose quantity, geometry, and characteristicsdepend on the experiment typology. Each tray hosts four carriers (Fig. 11.14) sealedwith optical windows or kept open to the space environment. The trays have amechanical interface to the structure and comply with the design of the lids. Thetrays are electrically connected to the structure by matable/dematable connectors.The sample carriers are designed to accommodate a number of optical filters

(neutral density and/or cutoff) to control wavelength and amount of incident light;they are also complemented with passive radiation dosimeters, such as thermolu-minescent detectors. Two or three control layers are foreseen in each carrier.In the flight of EXPOSE-R, tray 1 is dedicated to the AMINO and ORGANICS

experiments (Table 11.8). It is the only one not equipped with shutters, and itssample carriers are not covered with windows. It hosts pressurized and ventedsample cells, protected with 1- or 2-mm thick MgF2 windows (8 mm in diameter)(Fig. 11.15A). Both experiments have a dark control layer underneath the exposedset. Peculiarities of this tray include temperature sensors inside some cells (incontact with the inner window) and innovative design concepts for the pressurizedcells of the two experiments.Trays 2 and 3 (Fig. 11.15B, C) are dedicated to the samples of the so-called ROSE

(Response of Organisms to Space Environment) consortium, a team of biologistswhose experiments are part of a coordinated research effort (Table 11.8). The trayshost vented and sealed units, but here the sample carriers are always closed with an8-mm thick MgF2 window.The pressurized compartments carry experiments with a predefined gaseous

environment, provided during the integration of the scientific payload. Thisatmosphere has to be maintained during all mission phases (transportation tothe launch site, storage, trays’ integration into EXPOSE-R, launch, in-orbit oper-ations, retrieval, landing, and transportation to the de-integration site).The venting of the other compartments is achieved with motor-driven venting

valves that allow depressurization once in orbit and upon reception of a commandissued from the ground. Every EXPOSE-R tray is provided with this system, butonly specific sample carriers are connected to it.

11.3 Exposure Facilities for Astrobiology Experiments 299

Fig. 11.14 One of the three trays of EXPOSE; photo of theEngineering Model (courtesy of ESA).

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Fig. 11.15 Arrangement of the subunits of the EXPOSE traysaccording to the different experiment requirements. (A) Trayfor the experiments AMINO and ORGANICS; (B) tray for theexperiments ROSE 1, 2, 3, 4, and 8; (C) tray for the experimentsROSE 1, 2, 3, 4, 5, and R3D (courtesy of ESA).

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Because the only access to the sealed compartments is through the removal ofthe glass window, integration of the scientific payload has to be done inside a glovebox, in sterile or environment-controlled conditions.

11.3.3.4 EXPOSE-R and EXPOSE-EFor EXPOSE-R, the EXPOSE Engineering Model, used for the design and qual-ification of the EXPOSE Flight Model (called EXPOSE-E), has been upgraded toflight standards and made compatible with the interfaces and the operationalaspects of the external platforms of the Russian segment of the ISS (Fig. 11.16).The target launch date is October 2007, with an unmanned Progress cargo fromBaikonour. EXPOSE-E will fly with Columbus.For both missions, the integration of the facility on the external platforms (and

the removal of the experiment samples at exposure conclusion) will be done viaextravehicular activity, but the operational scenarios will be quite different. InEXPOSE-R, the experiment trays will be removed at mission completion (plannedafter one year in space), put in sealed transport containers, and, after a temporarystorage inside the RS-ISS, will be downloaded to the Earth onboard a Soyuz reentrycapsule. The facility will remain outside the ISS and might then be “refilled” with anew set of trays uploaded with the next Progress cargo. Such an “extended” missionis actually envisaged by the astrobiology scientific community in order to useEXPOSE as test bed for experiments, sensor packages, and new technologies tobe developed in the frame of the upcoming ExoMars mission (see Chapter 12).EXPOSE-E is planned to stay in orbit for about three years. It will be part of the

EUTEF, an assembly of ESA technology demonstration and scientific instruments,and as such, it will have to be dismounted together with it. Because it is the first tohave been developed, EXPOSE-E is not provided with removable experiment trays;

11.3 Exposure Facilities for Astrobiology Experiments 301

Fig. 11.16 Location of EXPOSE-R at the Russian moduleof the ISS (RS-ISS).

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therefore, its flexibility in accommodating new experiment samples and/or upgrad-ing is quite limited.EXPOSE-E will be mounted on one of the four external balconies of the Columbus

module, on the ISS (Fig. 11.17). Initially designed in combination with a coarsepointing device that would have allowed a longer direct orientation to the sun, ithad to be reconfigured for a less ambitious location on the Columbus starboard-oriented external platform, as part of the EUTEF assembly (Fig. 11.17).

11.3.3.5 Process of Experiment Proposal, Acceptance, Preparation, and ValidationThe experiment preparation process for this kind of research generally starts with arequest formulated by the scientists in the form of an unsolicited proposal or inreply to a dedicated Announcement of Flight Opportunity (AO) issued by the ESA.These AOs are published taking into account the interest and demand of scientificresearch in certain fields as well as the existing flight opportunities in terms ofavailable payloads and retrievable carriers.Once submitted, the experiment proposals are evaluated and rated by an in-

dependent peer review board. The preliminary selected experiments then undergoa detailed engineering assessment on their technical feasibility and on theircompatibility with facility characteristics and mission scenarios under the lead ofESA. Finally, the experiment complement is frozen.After being selected, the experiments undergo a dedicated program of verifica-

tion and qualification in order to achieve the necessary flight readiness. Thisnormally includes

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Fig. 11.17 Location of EXPOSE-E at the outer platform EUTEFon the European module Columbus of the ISS.

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• selection of samples,• environmental tests (UV, ionizing radiation, vacuum, etc.),• flight qualification tests (vibration, thermo-vacuum, thermo-

cycling),• material compatibility tests, and• experiment sequence tests (pre-mission).

The test results are used as feedback into the experiment hardware design process.For EXPOSE-R, an Experiment Verification Test Program (EXPOSE-EVT) is

established that includes the following elements:• assessment of the desiccation and UV radiation resistance of

the different species of ROSE in order to select suitableorganisms for the flight;

• determination of the acceptable temperature ranges;• assessment of the biocompatibility of the different samples;• selection of analytical methods for the different biological

endpoints to be investigated;• testing of sample preparation techniques for the space ex-

periment;• assessment of the resistance to polychromatic UV radiation;• definition of the optical requirements;• measurement of dose-effect curves to UV effects in order to

choose suitable filter combinations for the flight unit;• optimization of analytical methods for the different biological

endpoints adapted to the small sample volumes required bythe space hardware.

11.4Results from Astrobiology Experiments in Earth Orbit

Since the Apollo missions, European scientists have been involved in exobiologicalor radiation biology experiments in space. Table 11.10 shows the chronologies ofESA missions relevant to astrobiology.

Table 11.10 Missions in low Earth orbit relevant to astrobiology.

Year Spacecraft Experiment

1983 Spacelab 1 ES029: Response of resistant microbial system(Bacillus subtilis spores) to free space

1984–1990 LDEF Facility Exostack: Long-term survival of spores in space1992–1993 EURECA-ERA Exposure of different biological systems and complex

organic residues to selected parameters of outer space

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Year Spacecraft Experiment

1993 Spacelab D2 UVRAD: Biological responses to extraterrestrial solarultraviolet radiation and space vacuum

1993–2005 Foton/BIOPAN 25 experiments on 5 missions2003 BIOBOX-5/STS-107 RADCELLS: Effects of cosmic radiation in cells2004–2005 ISS MATROSHKA-1: Depth-dose distribution in a

human phantom2006–Future ISS EXPOSE-E, EXPOSE-R, MATROSHKA-2

11.4.1Relevance of Extraterrestrial Organic Molecules for the Emergence of Life

Primary organic chemistry first occurs in the interstellar medium. The chemicalprocesses by which these organic molecules are formed in the interstellar me-dium are mainly gas-phase ion–molecule reaction paths, which start with themost abundant molecule, hydrogen (H2), reacting with various ions. The proc-esses include hot and suprathermal reactions, photochemical processes, andsurface reactions on interstellar dust grains with successive evaporation. Whenin the course of pre-stellar evolution a molecular cloud becomes cooler (10–20 K)and denser (106 cm–3), trace molecules such as CO, H2O, CH3OH, and NH3

condense onto grain surfaces as ice mantles. In the cyclic evolutionary modelfor interstellar dust, developed by J. M. Greenberg, interstellar dust grains consistof a silicate core and a mantle of relatively nonvolatile higher-molecular-weightorganic compounds. Each complete cycle takes about 108 years, and the meanlifetime for an interstellar grain is about 5 · 109 years before it is consumed bystar formation. During the EURECA mission of ESA, in the Exobiology RadiationAssembly (ERA), such complex organic residues, produced in the laboratory, wereexposed to the full spectrum of solar UV, including vacuum UV radiation, inorder to simulate the photolytic processes thought to occur during chemicalevolution of interstellar grains. The exposure of the organic residue to solar UVfor about six months provided a total fluence of UV that is equivalent to thephoton fluence received within about 10 million years in the diffuse clouds of theinterstellar medium. Hence, the solar UV-irradiated samples of the EURECAmission were expected to resemble the interstellar organic mantles, which haveundergone at least one complete evolutionary cycle. Analysis of the samples afterretrieval showed that the UV-irradiated samples had changed in color from yellowto brown, indicating an increase in carbonization. Infrared spectra showed thatthe 3.4-�m feature of the samples matched quite well with the spectra of theinterstellar medium, thereby supporting the cyclic evolutionary model for inter-stellar dust.Studies in low Earth orbit have also contributed to answer the question of

whether the precursors of life were produced on the primitive Earth or transported

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to the early Earth via meteorites. The study of micrometeorites collected in theGreenland and Antarctic ice sheets by M. Maurette shows that the Earth capturesinterplanetary dust as micrometeorites at a rate of about 50–100 tons per day.About 99% of this mass is carried by micrometeorites in the 50–500 �m size range.In the Antarctic micrometeorites, a high percentage of unmelted chondritic micro-meteorites from 50 to 100 �m in size have been observed, indicating that a largefraction crossed the terrestrial atmosphere without drastic thermal treatment. Inthis size range, the carbonaceous micrometeorites represent 80% of the samplesand contain 2% of carbon on average. They might have brought about 3 · 1019 g ofcarbon over a period of 300 million years corresponding to the late terrestrialbombardment phase. This delivery represents more carbon than that engaged inthe surface biomass of the Earth, which amounts to about 1018 g. Amino acids suchas �-amino isobutyric acid have been recently identified in these Antarctic micro-meteorites. These grains contain a high proportion of metallic sulfides, oxides, andclay minerals that have catalytic capabilities. In addition to the carbonaceousmatter, micrometeorites might have delivered a rich variety of catalysts havingperhaps acquired specific crystallographic properties during their synthesis in themicrogravity environment of the early solar nebula. They may have functioned astiny chondritic chemical reactors when reaching oceanic water.Space environment alters the composition, morphology, and dynamics of these

interplanetary dust particles (IDPs) by processes such as thermal annealing,radiation and ion bombardment, or collisions. In the last years, techniques havebeen developed to collect IDPs in space. The advantage of this type of collection –compared to sampling on Earth – is that the samples are not altered by atmosphericentry effects. Passive aerogel collectors have been exposed on NASAs Long Dura-tion Exposure Facility (LDEF) and the MIR station, in order to collect grainsuncontaminated by interaction with Earth’s atmosphere or environment, andreturned to Earth. Aerogel collectors were used on the NASA Stardust mission tocollect and return to Earth grains from the interplanetary medium and from thecoma of comet Wild 2.Amino acids like those detected in the Murchison meteorite have been exposed

for 10 days to space conditions in Earth orbit during three months onboard MIR(PERSEUS experiment) and for about two weeks within the ESA facility BIOPANonboard the unmanned Russian satellites Foton 8 and Foton 11. They were exposedto the full spectrum of solar extraterrestrial UV radiation, including vacuum UV,and to space vacuum under different exposure conditions: either as free amino acidor associated with mineral powder. Analysis of the samples after flight showed thatexposed amino acids (aspartic acid and glutamic acid) were partially photo-proc-essed during their stay in space. However, decomposition was prevented when theamino acids were embedded in clays (see Chapter 1). The main limitations of theseexperiments were the relatively weak irradiation of the samples (because of theshort flight duration), the non-synchronous orbits, and the absence of an automaticsun pointing device. ESA’s EXPOSE facility onboard the ISS offers an interestingopportunity for long-duration exposure of amino acids and other biogenic mole-cules (see Section 11.3.3.).

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11.4.2Role of Solar UV Radiation in Evolutionary Processes Related to Life

Space experiments using solar UV radiation as the authentic energy sourcerepresent new approaches towards our understanding of the evolution of lifeand potential evolutionary steps on other celestial bodies. They may especiallycontribute to tackle the following issues:

• the formation and stability of organic molecules in the pre-biotic environment of early Earth;

• the role of the ozone layer in protecting life on Earth; and• the role of solar UV radiation in the planets and moons of

astrobiological interest, such as Mars, Saturn’s moon Titanand Jupiter’s moon Europa.

11.4.2.1 Efficiency of the Stratospheric Ozone Layer to Protect Our BiosphereUntil recently, assessment of the consequences of increasing environmental UV-Birradiation – caused by a decreasing concentration of stratospheric ozone, the so-called ozone hole – on the biosphere was based merely onmodel calculations. In anexperiment onboard the German Spacelab D2 mission that used extraterrestrialsolar UV radiation as natural radiation source and optical filters, the terrestrial UVradiation climate was simulated at different ozone concentrations down to very lowozone values, thereby using space as a kind of time machine. Biologically effectiveirradiances as a function of the simulated ozone column thickness were measuredwith Bacillus subtilis spores immobilized in a biofilm (Fig. 11.18). They werecompared to the expected irradiance, which was obtained from radiative transfercalculations multiplied with the biofilm action spectrum (an action spectrum givesthe spectral efficiency of UV radiation with regard to a certain biological effect,here, cell killing). After the mission, the biofilms were incubated and stained, and

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Fig. 11.18 Location of the experimentUV-RAD in the cargo bay of the Space Shuttleduring the German Spacelab D2mission (photocredit: DLR).

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optical densities indicative of the biological activity were determined for eachexposure condition by image analysis. It was found that with decreasing (simu-lated) ozone concentrations, the biologically effective solar UV irradiance stronglyincreased. The full spectrum of extraterrestrial solar radiation led to an incrementof the biologically effective irradiance by nearly three orders of magnitude com-pared to that of the solar spectrum at the surface of the Earth for average total ozonecolumns.Experiments with bacterial endospores, simulating the UV radiation climate of

Mars, were performed using the BIOPAN facility of ESA onboard a Foton satellite.These experiments tackled the question of the toxicity of the Martian regolith toterrestrial microorganisms exposed to the UV radiation climate of Mars. Thisinformation is pivotal for assessing the habitability of the surface of Mars andfor planetary protection efforts.

11.4.3Chances and Limits of Life Being Transported from One Body of Our Solar Systemto Another or Beyond

The idea of interplanetary transfer of life was originally put forward independentlyby three scientists: Richter in 1865, Lord Kelvin in 1894, and Svante Arrhenius in1903. The theory of “panspermia” as postulated by Arrhenius in 1903 holds thatreproductive bodies of living organisms can exist throughout the Universe anddevelop wherever the environment is favorable. This theory implies that duringthe evolution of the Universe, conditions favorable to the development of life haveprevailed at different locations and at different times. For example, early in thedevelopment of our Solar System, at a time when conditions on the young Earthmay have been hostile to the development of life, conditions conducive to thedevelopment of living systems may have existed simultaneously on other bodieseither within our Solar System (such as Mars, Venus, Jupiter’s moon Europa, orSaturn’s moon Titan) or within other solar systems. The panspermia theory doesnot set a precondition for terrestrial life having arisen on Earth; living organismscould well have arisen elsewhere in the Solar System (or Universe) and beentransported to Earth, where they encountered environmental conditions favorableto growth, proliferation, and eventual evolution into more-complex forms. Onceestablished, life on Earth would then be subject to transfer to other celestialbodies.Since its formulation, the theory of panspermia has been subjected to several

criticisms, with arguments such as: (1) it cannot be experimentally tested, (2) itshunts aside the question of the origin of life, and (3) living organisms cannotsurvive long-time exposure to the hostile environment of space, especially vacuumand radiation. However, recent experimental evidence, summarized below, has ledto a reexamination of the feasibility of the notion of interplanetary transfer of livingmaterial, particularly microorganisms.The scenario of interplanetary transfer of life involves three basic hypothetical

steps:

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• the escape process, which comprises removal to space ofbiological material that has survived being lifted from thesurface to high altitudes;

• an interim state in space, which implies survival of the bio-logical material over time scales comparable with the inter-planetary or interstellar passage; and

• the entry process, where a non-destructive deposition of thebiological material on another planet is required.

It is not know with certainty whether panspermia is likely to have occurred in thehistory of the Solar System, or whether it is feasible at all, but additional support tothe idea of panspermia is given by a variety of recent discoveries, such as theMartian meteorites (see Chapter 8), the high UV resistance of microorganisms atthe low temperatures of deep space, and the recovery of viable spores after about sixyears of exposure in space (see Chapter 5).In laboratory experiments that simulate the impact of a meteorite as a feasible

process of ejecting material from a planet to reach escape velocity, the survival ofmicroorganisms residing inside of rocks has been proved. Once rocks have beenejected from the surface of their home planet, the microbial passengers face anentirely new set of problems affecting their survival, namely, exposure to the spaceenvironment. With space technology, a new tool is available for testing experimen-tally whether microorganisms are capable of surviving a hypothetical journey fromone planet to another. In order to study the survival of resistant microbial forms in

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Fig. 11.19 Space Simulation Facility (PSI) atthe Institute of Aerospace Medicine, DLR, forthe pre-flight testing of the experiments onEURECA and EXPOSE (photo credit: DLR).

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the upper atmosphere or in free space, microbial samples have been exposed in situby use of balloons, rockets, or spacecraft, and their responses were investigatedafter recovery. For this purpose, several facilities were developed, such as theexposure device on Gemini, MEED on Apollo, ES029 on SL1, ERA on EURECA,UV-RAD on Spacelab D2, and BIOPAN on Foton. These investigations weresupported by studies in the laboratory in which certain parameters of space(high and ultrahigh vacuum, extreme temperature, UV radiation of differentwavelengths, ionizing radiation) were simulated and the microbial responseswere determined (Fig. 11.19).

11.4.3.1 Effects of Space VacuumBecause of its extremely dehydrating effect, space vacuum has been argued to beone of the factors that may prevent interplanetary transfer of life. However, spaceexperiments have shown that up to 70% of bacterial and fungal spores survivedshort-term (up to 10 days) exposure to space vacuum, even without any protection.The chances of survival in space were increased if the spores were embedded inchemical protectants, such as sugars or salt crystals, or if they were exposed in thicklayers. For example, during the LDEF mission, 30% of B. subtilis spores survivednearly six years of exposure to space vacuum when embedded in salt crystals,whereas 80% survived in the presence of glucose. Sugar and polyalcohol stabilizethe structure of the cellular macromolecules, especially during vacuum-induceddehydration, leading to increased rates of survival. In addition, endolithic micro-organisms in nature are probably distributed in micro-cracks and pore spaceswithin rock as consortia biofilms embedded in a complex extracellular polysac-charide matrix, which would be expected to provide a degree of protection fromextreme vacuum. Recent studies on lichens under simulated space conditions andduring the BIOPAN-5 mission have demonstrated the high resistance of thesecommunities to space vacuum.To determine the protective effects of different meteorite materials, “artificial

meteorites” were constructed by embedding B. subtilis spores in clay, meteoritedust, or simulated Martian soil. Their survival was determined after exposure to thespace environment. Crystalline salt provided sufficient protection for osmophilicmicrobes to survive at least two weeks in space. For example, a species of thecyanobacterium Synechococcus that inhabits gypsum-halite crystals was capable ofnitrogen and carbon fixation. Concerning an extreme halophile microorganism,about 5% of a species survived after exposure to the space environment for twoweeks within the BIOPAN facility in connection with a Foton space flight.The mechanisms of cellular damage due to vacuum exposure are based on the

extreme desiccation imposed. If not protected by internal or external substances,cells in a vacuum experience dramatic changes in such important biomolecules aslipids, carbohydrates, proteins, and nucleic acids. Upon desiccation, the lipidmembranes of cells undergo dramatic phase changes from planar bilayers tocylindrical bilayers. The carbohydrates, proteins, and nucleic acids undergo so-called Maillard reactions, i.e., amino-carbonyl reactions, to give products that

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become cross-linked, eventually leading to irreversible polymerization of the bio-molecules. Concomitant with these structural changes are functional changesincluding altered selective membrane permeability, inhibited or altered enzymeactivity, decreased energy production, altered genetic information, etc. Vacuum-induced damage to DNA is especially dramatic because it may lead to death ormutation. During the Spacelab 1 mission, a 10-fold-increased mutation rate overthe spontaneous rate was observed in spores of B. subtilis after exposure to spacevacuum. This mutagenic effect by vacuum is probably based on a uniquemolecularsignature of tandem double-base changes at restricted sites in the DNA. Inaddition, DNA strand breaks have been observed to be induced by exposure tospace vacuum. Such damage would accumulate during long-term exposure tospace vacuum because DNA repair is not active in the desiccated state. Sporesurvival ultimately depends on the efficiency of DNA repair after rehydration andgermination.The high resistance of bacterial endospores to desiccation is due mainly to a

dehydrated core enclosed in a thick protective envelope, the cortex and the sporecoat layers, and the protection of their DNA by small proteins whose bindinggreatly alters the chemical and enzymatic reactivity of the DNA. However, thestrategies by which B. subtilis spores protect their integrity, including that of DNA,against vacuum damage are not yet fully understood. Non-reducing sugars, such astrehalose or sucrose, generally help to prevent damage to DNA, membranes, andproteins by replacing the water molecules during the desiccation process andthereby preserving the three-dimensional structure of the biomolecules. Althoughbacterial spores do not naturally accumulate the substances, the addition of glucoseto the spores substantially increases the survival rate of spores in space vacuum.

11.4.3.2 Effects of Extraterrestrial Solar UV RadiationSolar UV radiation has been found to be the most deleterious factor of space, astested with dried preparations of viruses and bacterial and fungal spores. Thereason for this is the highly energetic UV–C and vacuum UV radiation that isdirectly absorbed by the DNA, as demonstrated by action spectroscopy in space(Fig. 11.5). The full spectrum of extraterrestrial UV radiation kills unprotectedspores of B. subtilis within seconds, as discovered during the Spacelab 1 mission.These harmful UV ranges do not reach the surface of the Earth because they areeffectively absorbed by the Earth’s atmosphere. The photobiological and photo-chemical effects of extraterrestrial UV radiation are based on the production ofspecific photoproducts in the DNA that are highly mutagenic and lethal. The mostdamaging photochemical lesions in the DNA are thymine-containing dimers:cyclobutadipyrimidines, the (6–4) pyrimidine–pyrimidone adducts, and their Dew-ar valence isomer.If spores of B. subtilis were simultaneously exposed to solar UV radiation and

space vacuum, they responded with an increased sensitivity to a broad spectrum ofsolar UV (>170 nm) as well as to selected wavelengths. Upon dehydration, e.g., inspace vacuum, DNA undergoes substantial conformational changes. This conver-

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sion in the physical structure leads to altered DNA photochemistry, resulting in a10-fold increase in UV sensitivity of B. subtilis spores in space vacuum as comparedto spores irradiated at atmospheric pressure. The photoproducts generated withinthe DNA of B. subtilis spores exposed to UV radiation in vacuum were differentfrom those induced in wet spores; two thymine decomposition products, namely,the cis-syn and trans-syn cyclobutane thymine dimers, as well as DNA-protein cross-linking were found in addition to the spore photoproduct, the only photoproductinduced by UV in wet spores.

11.4.3.3 Effects of Galactic Cosmic RadiationAmong the ionizing components of radiation in space, the heavy primaries, the so-called HZE particles (see Section 11.1.1.1), are the most biologically effectivespecies. Because of their low flux (they contribute to approximately 1% of theflux of particulate radiation in space), methods have been developed to localizeprecisely the trajectory of an HZE particle relative to the biological object and tocorrelate the physical data of the particle relative to the observed biological effectsalong its path. In the BIOSTACK method (Fig. 11.20), visual track detectors aresandwiched between layers of biological objects in a resting state; one candidate isB. subtilis spores. This method allows us to

• localize each HZE particle’s trajectory in relation to the bio-logical specimens;

• investigate the responses of each biological individual hitseparately, with regard to its radiation effects;

• measure the impact parameter, which is the distance betweenthe particle track and the sensitive target;

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Fig. 11.20 BIOSTACK concept to measure the effects of singleheavy ions (HZE particles) of galactic cosmic radiation (GCR) inbiological systems in resting state (photo credit: DLR).

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• determine the physical parameters (charge [Z], energy [E],and linear energy transfer [LET]); and

• correlate the biological effect with each HZE particleparameter.

Taking the results from several BIOSTACK experiments in space (Apollo 16,Apollo 17, Apollo-Soyuz, Spacelab, EURECA) as well as those obtained at acceler-ators, one can draw the following general conclusions:

• The inactivation probability for spores, centrally hit, is sub-stantially less than 1.

• The effective radial range of inactivation around each HZEparticle, the so-called impact factor, extends far beyond therange where inactivation of spores by �-rays (secondary elec-tron radiation) can be expected.

• This far-reaching effect is less pronounced for ions of lowenergies (1.4 MeV per mass unit), a phenomenon that mayreflect the “thin-down effect” at the end of the ion’s path. Thedependence of inactivated spores from impact parameterpoints to a superposition of two different inactivation mech-anisms: a short ranged component reaching up to about1 �m that may be traced back to the �-ray dose (secondaryelectrons) and a long-ranged one that extends at least tosomewhere between 4 and 5 �m off the particle’s trajectoryfor which additional mechanisms are conjectured, such asshock waves, electromagnetic radiation, or thermophysicalevents.

The data show that B. subtilis spores would survive even a central hit of an HZEparticle of cosmic radiation to a certain extent. However, these HZE particles ofcosmic radiation are conjectured to set the ultimate limit on the survival of sporesin space because they penetrate even thick shielding. Because they interact with theshielding material by creating secondary radiation, with increasing shieldingthickness the dose rates go through a maximum. They reach their maximumbehind a shielding layer of about 10 cm; behind shielding of about 130 cm, thevalue is the same as obtained without any shielding, and only for higher shieldingthickness does the dose rate reduce significantly. Calculations based on the spaceexperiments have shown that if shielded by 2–3 m of meteorite material, a sub-stantial fraction of a spore population (about 100 from a population of 108) wouldsurvive the exposure to cosmic radiation, even after several million years in space.The same survival fraction would be reached after about 500 000 years without anyshielding and after 350 000 years with 1 m of shielding.These studies on the biological effects of the HZE fraction of cosmic radiation

are of interest for answering astrobiological questions, and they provide importantbasic information for our attempts to assess the radiation risks to humans inspace.

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11.4.3.4 Combined Effects of All Parameters of SpaceWith the LDEF mission, for the first time B. subtilis spores were exposed to the fullenvironment of space for an extended period of time (nearly six years), and theirsurvival was determined after retrieval (Fig. 11.21). The samples were separatedfrom space by a perforated aluminum dome only, which allowed access of spacevacuum, solar UV radiation including vacuum UV, and most of the components ofcosmic radiation. It was found that even in the unprotected samples thousands ofspores survived the space journey (from an initial sample size of 108 spores). Allspores were exposed in multilayer and pre-dried in the presence of glucose. Thespore samples had turned from white to yellow during the mission, a phenomenonthat is probably due to photochemical processes. It was suggested that all spores inthe upper layers were completely inactivated by the high flux of solar UV radiation.With time, they formed a protective crust that considerably attenuated the solar UVradiation for the spores located beneath this layer. Therefore, the survivors prob-ably originated from the innermost part of the samples.

11.4.3.5 Time Scales of Interplanetary Transport of LifeTo travel from one planet of our Solar System to another, e.g., from Mars to Earth,by random motion, a mean time of several hundred thousands to millions of yearshas been estimated for boulder-sized rocks but only two months for microscopicparticles. Therefore, the LDEF experiment may be considered a reasonable simu-lation of an interplanetary transfer event. Because LDEF was in a near-equatorial,low-altitude Earth orbit, during each orbit the satellite traveled about 40 650 kmevery 90 min. Thus, over the nearly six-year duration of the LDEF experiment, thesatellite traveled over 109 km, the approximate equivalent of the distance fromEarth to Saturn if it had been flying on a straight course rather than in an ellipticalorbit. The likelihood of spore survival over the time spans involved in interplan-etary transfer is therefore quite high.For future astrobiological research in space, ESA is developing the EXPOSE

facility that is to be attached to external pallets of the ISS for 1–3 years (see Section11.3.3). EXPOSE will support long-term in situ studies of microbes in artificialmeteorites, as well as of microbial communities from special ecological niches,such as endolithic and endoevaporitic ecosystems. These experiments on theResponses of Organisms to the Space Environment (ROSE) include the study of

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Fig. 11.21 Position of the Exostack experimenton the LDEF of NASA that stayed for nearly6 years in Earth orbit (photo credit: NASA).

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photobiological processes in simulated radiation climates of planets (early Earth,early and present Mars, and the role of the ozone layer in protecting the biospherefrom harmful UV-B radiation) as well as studies of the probabilities and limitationsfor life to be distributed beyond its planet of origin. Results from the EXPOSEexperiments will provide us with a better understanding of the processes regulatingthe interactions of life with its environment.A hypothetical scenario of interplanetary transfer of life requires that the micro-

organisms finally be deposited from space to a target planet. When captured by aplanet with an atmosphere, most meteorites are subjected to very high temper-atures during landing. However, because the fall through the atmosphere takesonly a few seconds, the outermost layers form a kind of heat shield and the heatdoes not reach the inner parts of the meteorite. During entry, the fate of themeteorite strongly depends on its size. Large meteorites may break into pieces;however, these may still be large enough to remain cool inside until hitting thesurface of the planet. Medium-sized meteorites may obtain a melted crust, whereasthe inner part still remains cool. Micrometeorites of a few micrometers in size maytumble through the atmosphere without being heated at all above 100�C. There-fore, it is quite possible that a substantial number of microbes can survive thelanding process on a planet. A first attempt to study the fate of microorganismsembedded inside a small meteorite was performed within the STONE experiment(Fig. 11.12) during the flight of the Foton satellite in 2005 (see Section 11.3.2).

11.4.4Radiation Dosimetry in Space

Measurements of radiation exposure in Earth orbit have been performed duringmanned and robotic space flights at various altitudes, orbital inclinations, dura-tions, periods during the solar cycle, and mass shielding (Fig. 11.22). Because of

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Fig. 11.22 Effective doses measured in low Earth orbit missionsand missions to the Moon (courtesy of G. Reitz, DLR).

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the complex mixture of radiations occurring in space, comprising sparsely ioniz-ing components (photons, electrons, pions, muons, and protons) and denselyionizing components (heavy ions, neutrons, and nuclear disintegration stars)(see Section 11.1.), different dosimetry systems have been applied that specificallyrespond to the quality of the radiation under consideration. However, mostdosimetric systems used provided data on the “surface” or skin dose only. Forradiation protection purposes, it is important to assess the depth-dose distributionwithin the human body and especially at the most radiation-sensitive organs, suchas the brain, the blood-forming organs, and the gonads. Therefore, humanphantoms equipped with different dosimetric systems at the sites of sensitiveorgans are required. The anthropomorphic phantom MATROSHKA is one suchexample; it was exposed for one year to the radiation in space outside of the ISS(Fig. 11.23) in order to determine the depth-dose distribution of radiations withinthe human body during EVAs. It consists of a human phantom upper torsocomposed of 33 slices equipped with passive and active radiation dosimeters atthe sites of different organs.

11.4 Results from Astrobiology Experiments in Earth Orbit 315

Fig. 11.23 Human phantom MATROSHKA (a) attached to theouter platform of the Russian module of the ISS during its one-year flight in 2005; (b) mounting during an extravehicular activity;(c) during disassembly inside the Russian segment of the ISS(photo credit: ESA, courtesy of G. Reitz, DLR).

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11.5Future Development and Applications of Exposure Experiments

The features of EXPOSE allow passive exposure of samples to space with contin-uous monitoring of the environmental conditions during the mission, in particularof UV radiation, broad solar spectrum, temperature, and residual pressure. Aspreviously described (see Section 11.3.3), predefined thermal conditions are guar-anteed during exposure by use of

• electrical heaters positioned under the trays and inside theframe structure;

• thermal blankets around the facility and around its supportstructure;

• low-conductive interfaces (Ti bolts/washers) between thefacility and EUTEF-CEPA; and

• coatings on the exposed surfaces with low absorbivity–highemissivity characteristics.

Temperature should be maintained within specific ranges (+5 to +15 �C or –20 to–5 �C) despite the environmental conditions. The strategy aims to avoid “crossing”of the freezing point. These thermal requirements are generally originated by theradiation biology experiments, where biological samples sensitive to large temper-ature variations are exposed to space radiation.On the contrary, astrobiology experiments try to simulate as closely as possible

the conditions experienced by organic matter when it is traveling with comets orasteroids or when exposed to extraterrestrial conditions. In this case, low temper-atures, far below 0�C, are desired, while maintaining a full exposition to the solarUV radiation. This is why a future evolution of a facility like EXPOSE should beprovided with some cooling devices, either passive, such as heat pipes and radiatorsconductively linked with the experiment trays, or semi-active, such as thermo-electric junctions (Peltier) linked to heat exchangers.The onboard sensor packages, including active radiation measurement devices

capable of correlating input data with time (a prototype, Radfet, flew with BIOPAN-5in May 2005), could be improved. In addition, Sun pointing devices and samplecompartments with embedded temperature sensors are part of future development.EXPOSEmight be used in the near future as a “test bed” for experiments in support

of the upcoming planetary exploration missions. The design and development of amobile exobiology package (Pasteur) to be operated on the Martian surface (ExoMarsmission) (see Chapter 12) will most probably require testing of materials, electroniccomponents, andmechanical devices that will have to be operated continuously whenexposed for a long time to extraterrestrial conditions (low pressure or vacuum, largetemperature variations, high radiation, electric and magnetic fields, etc.).Looking at the near-term plans of ESA for Mars exploration, it is clear that the

first missions (ExoMars Pasteur, Mars Sample Return) will bring to the Martiansurface a set of instrumentation sterilized of terrestrial microorganisms andcleansed of Earth organic agents, in an attempt to avoid any contamination

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whenmeasuring and investigating theMartian soil characteristics. These planetaryprotection issues are being investigated at the moment (see Chapter 13). Thesestudies may require the help of an exposure platform like EXPOSE for validation,qualification, and testing of materials or technical devices.The second phase of the exploration program of ESA foresees that life and

organic matter will be brought to Mars in support of human activities on Mars.In this case, EXPOSE or EXPOSE-like facilities may be used for the understandingof non-terrestrial environment effects on organic matter. ISS external platformsprovide unique environmental conditions, different from those of Earth and Mars,that allow testing and verifying the effects of specific parameters of outer space,applied singly or in combination.

11.6Further Reading

11.6.1Books and Articles in Books

B�cker, H., Horneck, G. Studies on the effectsof cosmic HZE particles in different biolog-ical systems in the Biostack experiments Iand II, flown on board of Apollo 16 and 17.In Radiation Research, Nygaard, O. F., Adler,H. I., Sinclair, W. K. (Eds.), Academic Press,New York, pp. 1138–1151, 1975.

ESA, The ESA Radiation Handbook, ESA PSS-01–609 Issue 1, 1993.

ESA, Proceedings of the 2nd European Symposiumon the Utilization of the International SpaceStation, ESTEC, Noordwijk, The Nether-lands, 16–18 November 1998, ESA SP-433,1999, with the following articles:– Brack, A., Ehrenfreund, P., Otroshenko,V., Raulin, F. From interstellar chemistryto terrestrial life: exposure experiments inEarth orbit, pp. 455–458.

– Horneck, G., Wynn-Williams, D. D.,Mancinelli, R. L., Cadet, J., Munakata, N.,Ronto, G., Edwards, H. G.M., Hock, B.,W�nke, H., Reitz, G., Dachev, T., H�der,D. P., Brillouet, C. Biological experimentson the EXPOSE facility of the Interna-tional Space Station ISS, pp. 459–468.

Feuerbacher, B., Stoewer, H. (Eds.),Utilizationof Space – Today and Tomorrow, Springer,Berlin Heidelberg, 2006

Horneck, G., Brack, A. Study of the origin,evolution and distribution of life withemphasis on exobiology experiments in

Earth orbit. In Advances in Space Biologyand Medicine, Vol. 2, Bonting, S. L. (Ed.),JAI Press, Greenwich, CT, pp. 229–262,1992.

Horneck, G. The Biostack concept and itsapplication in space and at accelerators:studies on Bacillus subtilis spores. In Biolog-ical Effects and Physics of Solar and GalacticCosmic Radiation, Part A, Swenberg, C. E.,Horneck, G., Stassinopoulos, E. G. (Eds.)Plenum Press, New York, pp. 99–115, 1993.

Horneck, G., Baumstark-Khan, C., Reitz, G.Space microbiology: effects of ionizingradiation on microorganisms in space. InThe Encyclopedia on Environmental Microbi-ology, Bitton, G. (Ed.), Wiley, New York,pp. 2985–2996, 2002.

Innocenti, L., Mesland, D. (Eds.) EURECAScientific Results, Adv. Space Res. Vol. 16,No. 8, Pergamon, Oxford, 1995, especiallythe following articles:– Dose, K., Bieger-Dose, A., Dillmann, R.,Gill, M., Kerz, O., Klein, A., Meinert, H.,Nawroth, T., Risi, S. Stridde, C. ERAexperiment “Space Biochemistry” pp.(8)119–(8)129.

– Horneck, G., Eschweiler, U., Reitz, G.,Wehner, J., Willimek, R., Strauch, K.Biological responses to space: results ofthe experiment “Exobiological Unit” ofERA on EURECA I. pp. (8)105–(8)118.

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Maurette, M. Micrometeorites and the Mys-teries of our Origins, Springer, Berlin Hei-delberg New York, 2006.

Moore, D., Bie, P., Oser, H. (Eds.) Biological andMedical Research in Space, Springer, Heidel-berg, 1996, especially the following articles:– Kiefer, J., Kost, M., Schenk-Meuser, K.Radiation biology, pp. 300–367.

– Horneck, G. Exobiology, pp. 365–431.

Seibert, G. A World without Gravity –Researchin Space for Health and Industrial Processes,ESA SP-1251, ESA-ESTEC, Noordwijk, TheNetherlands, 2001, available online:http://www.esa.int/esapub/sp/sp1251/sp1251web.pdf.

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11.6.2Articles in Journals

Barbier, B., Chabin, A., Chaput, D., Brack, A.Photochemical processing of amino acidsin Earth orbit, Planet. Space Sci. 1998, 46,391–398.

Brack, A., Baglioni, P., Borruat, G., Brand-st�tter, F., Demets, R., Edwards, H. G.M.,Genge M., Kurat, G., Miller, M. F., Newton,E.M., Pillinger, C. T., Roten, C.-A., Wasch E.Dometeoroids of sedimentary origin surviveterrestrial atmospheric entry? The ESA arti-ficial meteorite experiment STONE, Planet.Space Sci. 2002, 50, 763–772.

Demets, R., Schulte, W., Baglioni, P. The past,present and future of BIOPAN, Adv. SpaceRes. 2005, 36, 311–316.

Facius, R., Reitz, G., Sch�fer, M. Inactivationof individual Bacillus subtilis spores in de-pendence on their distance to single cosmicheavy ions, Adv. Space Res. 1994, 14 (10),1027–1038.

Ferrini, G., Colangeli, L., Palumbo, P., West-phal, J. A., Borg, J. Capture experiments ofmeteoroids and space debris in LEO: recentresults and future possibilities, Microgravityand Space Station Utilisation 2001, 2, 2–4.

Greenberg, J. M. Approaching the interstellargrain organic refractory component. Astro-phys. J. 1995, 455, L177.

Horneck, G. Responses of Bacillus subtilisspores to space environment: Results fromexperiments in space, Origins Life Evol.Biosph. 1993, 23, 37–52.

Horneck, G. Exobiological experiments inEarth orbit, Adv. Space Res. 1998, 22(3),317–326.

Horneck, G. European activities in exobiologyin Earth orbit: results and perspectives, Adv.Space Res. 1999, 23, 381–386.

Horneck, G., B�cker, H., Reitz, G., Requardt,H., Dose, K., Martens, K. D., Menning-

mann, H. D., Weber, P. Microorganisms inthe space environment, Science 1984, 225,226–228.

Horneck, G., B�cker, H., Reitz, G. Long-termsurvival of bacterial spores in space, Adv.Space Res. 1994, 14 (10), 41–45.

Horneck, G., Rettberg, P., Rabbow, E., Strauch,W., Seckmeyer, G., Facius, R., Reitz, G.,Strauch, K., Schott, J. U. Biological dosime-try of solar radiation for different simulatedozone column thicknesses, J. Photochem.Photobiol. B: Biol. 1996, 32, 189–196.

Mancinelli, R. L., White, M. R., Rothschild, L. J.BIOPAN survival I: exposure of the osmo-philes Synechococcus sp. (Nageli) and Hal-oarcula sp. to the space environment. Adv.Space Res. 1998, 22(3), 327–334.

Mileikowsky, C., Cucinotta, F., Wilson, J.W.,Gladman, B., Horneck, G., Lindegren, L.,Melosh, J., Rickman, H., Valtonen, M.,Zheng, J. Q. Natural transfer of viable mi-crobes in space, Part 1: From Mars to Earthand Earth toMars, Icarus 2000, 145, 391–427.

Nicholson, W. L., Munakata, N., Horneck, G.,Melosh, H. J., Setlow, P. Resistance of Ba-cillus endospores to extreme terrestrial andextraterrestrial environments, Microb. Mol.Biol. Rev. 2000, 64, 548–572.

Obe, G., Johannes, I., Johannes, C., Hallmann,K., Reitz, G., Facius, R. Chromosomalaberrations in blood lymphocytes of astro-nauts after long-term space flights, Int. J.Radiat. Biol. 1997, 72, 726–734.

Reitz, G., Beaujean, R., Heckeley, N., Obe, G.Dosimetry in the space radiation field,. Clin.Investig. 1993, 71, 710–717.

Rettberg, P., Horneck, G. Biologically weightedmeasurement of UV radiation in space andon Earth with the biofilm technique, AdvSpace Res. 2000, 26, 2005–2014.

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11.6.3ESA Online Archives

Erasmus Experiment Archive, all ESA ex-periments in microgravity with details andpublications: spaceflight.esa.int/eea

ESA ISS Spaceflight Users Web site: single-stop shop for all scientific utilization–relatedissues: spaceflight.esa.int/users

European User Guide to Low Gravity Plat-forms: The reference document for Scien-tific and Technical Users:http://spaceflight.esa.int/users/index.cfm?act=default.page&level=1c&page=2130

Web Streaming Network: all AstrobiologyCourse Network lectures are available inQuickTime (300 kbps) as streaming videoon-demand with synchronized slides:streamiss.spaceflight.esa.int

Erasmus Virtual Campus E-Learning tool: allAstrobiology Course Network lectures areavailable within the Erasmus User CentreiLinc tool, user ID and password available onrequest: isslinc.spaceflight.esa.int/virtual

ESA Space Radiation and Effects:http://space-env.esa.int/index.html

11.7Questions for Students

Question 11.1The space environment in low Earth orbit is quite similar to that of deep space.

Describe the main differences between the two environments.Question 11.2Describe the main current flight opportunities for astrobiology experiments

offered by the European Space Agency and the scientific aims pursued.Question 11.3What are the effects of UV radiation (extraterrestrial and terrestrial) on living

systems? Describe the physical, chemical, and biological interactions and thespectral dependence of the effects.Question 11.4Describe the interaction between the Earth’s magnetosphere, the incoming

galactic cosmic radiation, and the radiation originating in the Sun.Question 11.5Describe an astrobiology experiment for one of the two experiment carriers of the

European Space Agency (EXPOSE or BIOPAN), its scientific objectives, and how torealize them.

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12Putting Together an Exobiology Mission: The ExoMars ExampleJorge L. Vago and Gerhard Kminek

In this chapter, the different steps towards the making of anexobiological mission to Mars are presented, exemplified by theExoMars project of the European Space Agency (ESA). The chapterstarts with a short description of the exobiological activities at ESAthat have led to the development of the ExoMars concept. Then, thescientific rationale and objectives of the mission are covered,followed by a description of the instruments and engineeringdesign required to reach the objectives. It is pointed out thatbesides a strong science case and a feasible engineering concept,programmatic and financial boundaries play a major role inshaping a mission.

12.1Background of the ExoMars Mission

12.1.1Searching for Life on Mars

The term exobiology, in its broadest definition, denotes the study of the origin,evolution, and distribution of life in the Universe. It is well established that lifearose very early on the young Earth. Fossil records show that life had alreadyattained a large degree of biological sophistication 3.4 billion years ago (see Chapter1). Since then, it has proven extremely adaptable, colonizing the most disparateecological niches, from the very cold to the very hot, and spanning a wide range ofpressure and chemical conditions (see Chapter 5). For organisms to have emergedand evolved, water must have been readily available on our planet. Life as we knowit relies, above all else, upon liquid water. Without it, the metabolic activities ofliving cells are not possible. In the absence of water, life either ceases or slips intoquiescence.Mars today is cold, desolate, and dry. Its surface is oxidized and exposed to

sterilizing and degrading ultraviolet (UV) radiation. Low ambient temperature and

12.1 321

Complete Course in Astrobiology. Edited by Gerda Horneck and Petra RettbergCopyright � 2007 WILEY-VCH Verlag GmbH & Co. KGaA, WeinheimISBN: 978-3-527-40660-9

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pressure preclude the existence of liquid water – except, perhaps, in localizedenvironments, and then only episodically. Nevertheless, numerous features,such as large channels, dendritic valley networks, gullies, and sedimentary rockformations, suggest the past action of surface liquid water on Mars – and lots of it.The sizes of Martian outflow channels imply immense discharges, exceeding anyfloods known on Earth (see Chapter 8).Mars’s observable geological record spans approximately 4.5 billion years. From

the number of superposed craters, the oldest terrain is believed to be about 4 billionyears old and the youngest possibly less than 100 million years. Most valley net-works are ancient (3.5–4.0 billion years old), but as many as 25–35% may be morerecent. Today, water on Mars is stable only as ice at the poles, as permafrost inwidespread underground deposits, and in trace amounts in the atmosphere. Froma biological perspective, past liquid water itself motivates the question of life onMars. If Mars’s surface was warmer and wetter for the first 500 million years of itshistory, perhaps life arose independently there, at more or less the same time as itdid on Earth.An alternative pathway may have been the transport of terrestrial organisms

embedded in meteoroids, delivered from Earth to Mars. Yet another hypothesis isthat life may have developed within a warm, wet, subterranean environment. Infact, given the discovery of a flourishing biosphere 1 km or more below Earth’ssurface, a similar vast microbial community may be active on Mars, having longago retreated into that ecological niche following the disappearance of a morebenign surface environment. The possibility that life may have evolved on Marsduring an earlier period when water existed on its surface, and that organisms maystill exist underground, marks the planet as a prime candidate to search for lifebeyond Earth.

12.1.2Exobiology Research at ESA

Exobiology activities at ESA started in the 1980 s with the preparation of experi-ments for the Exobiology and Radiation Assembly (ERA). ERA flew in 1992,onboard the European Retrievable Carrier mission, and was active for almost ayear. It provided results on the exposure of invertebrates, microorganisms, andorganic molecules to long-term space conditions, such as UV radiation, cosmicradiation, and vacuum (see Chapter 11).Other experiments were conducted using BIOPAN, a facility externally attached

to the Russian Foton retrievable satellite. BIOPAN’s upper shell is a motor-drivenlid that opens when in orbit to expose its samples to space. At the end of its 10-daymission, the lid is closed. To withstand the extreme heat of reentry, the entireBIOPAN structure is protected by an ablative heat shield; upon landing, thespecimens can be retrieved and examined. Five flights took place, in 1992, 1994,1997, 1999, and 2005. Microbes, seeds, and organic molecules were subjected to theharsh low Earth orbit environment in different manners, such as with and withoutradiation protection, in space vacuum, or in the presence of a simulated atmos-

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phere. The response of the samples was determined. It was found that unprotectedbacterial spores were completely or nearly totally inactivated by the UV radiation.Thin layers of clay, rock, or meteorite material were successful in UV shieldingonly when they were in direct contact with the spores. Thus, concerning a possiblescenario for the interplanetary transfer of life, the BIOPAN data suggest that smallrock ejecta of a few centimeters in diameter may provide sufficient protection fororganisms to survive the space journey. However, micron-sized grains, as invokedin some panspermia theories, would most likely prove inadequate (see Chapter 11).Meteorites may be natural vehicles for transporting resistant life forms across

space. Hence, also on Foton, suitable meteorite analogues, the STONE experi-ments, were subjected to the searing environment of spacecraft reentry. The firstthree rock samples were fixed to the Foton capsule’s heat shield and recovered forstudy upon landing in 1999. The goal was to investigate why, among the knownmeteorites believed to have come from Mars, none is of sedimentary origin. Cansedimentary rocks survive reentry? Are they altered beyond recognition by theirpassage through the Earth’s atmosphere? STONE provided valuable results on thephysical and chemical modifications undergone by sedimentary rocks duringatmospheric infall. The 2005 mission contained four rock specimens, this timealso including microorganisms. The goal of this work was to simulate a meteorite’satmospheric impact and to observe to what degree the embedded microorganismswere affected (see Chapter 11).From 2007 onwards, the ESA facility EXPOSE will be mounted on an external

payload site of the International Space Station (ISS). Carefully controlled param-eters, such as space vacuum and well-defined wavebands of solar UV and cosmicradiation, will act on the samples, which can be combined with chemical and/orphysically protective agents. This will help to elucidate whether, and to what extent,meteoritic material may offer enough protection for life to remain viable after along permanence in space. It will also allow the study of long-term survivability anddamage/repair mechanisms operating in microorganisms under space conditions.Finally, EXPOSE will shed light on space chemistry in the Solar System in relationto the origin of life. Organic molecules of biological interest, such as amino acids,peptides, and nucleic acids, will be exposed to characterize any variations in theirstability and reactivity. Additionally, powders of clay, meteorite, and terrestrial rockwill be used to model the mineral fraction present in meteoroid and interstellardust to understand their effect as filters or as potential catalysts (see Chapter 11).Other ESA initiatives that will contribute to our knowledge of important pre-

biotic chemical processes are the cometary mission Rosetta and the Huygens probeof the Cassini–Huygens mission. Rosetta will be the first mission to orbit and landon a comet. For this, the comet 67P/Churyumov-Gerasimenko has been chosen. Itwill collect essential information to help us understand the formation and evolu-tion of our Solar System. Rosetta will also help us to determine whether cometscould have contributed to the origin of life on Earth by seeding our planet withcomplex organic molecules through impacts. Light, volatile substances carried bycomets also may have played an important role in the formation of Earth’s oceansand atmosphere (see Chapter 3).

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ESA’s Huygens probe, traveling to Titan aboard NASA’s Cassini spacecraft, suc-cessfully completed its mission in 2005 (see Chapter 9). Many scientists considerthat the present composition of Titan’s atmosphere – mainly nitrogen and methane– might closely resemble that of early Earth, before life began on our planet.Throughout its 2.5-h descent,Huygensmade a detailed study of Titan’s atmosphereand characterized its surface in the proximity of the landing site. Ultraviolet radia-tion from the Sun breaks methane molecules apart to produce a thick layer of smogat middle altitudes. An organic rain of methane and nitrogen containing aerosolsfalls steadily onto the satellite’s surface, creating an Earth-like terrain that includesextended river networks. The results ofHuygens reveal the uniqueness of Titan in theSolar System as a planetary-scale laboratory for studying prebiotic chemistry.The Russian Mars ’96 mission consisted of an orbiter, two landers, and two

penetrators to perform subsurface measurements. It was launched in November1996, but because of a failure in the rocket’s upper stage, it fell back to Earth.European scientists had contributed many instruments to Mars ’96. With nopossibility of a Russian reflight, in 1997, within the Space Science Program ofESA, work was started on the design and development of the first ESA spacecraft tovisit another planet: Mars Express. Mars Express, comprising an orbiter and theBeagle 2 lander, was launched in 2003 using a Soyuz rocket. Presently in operation,the mission addresses a wide variety of scientific objectives, concentrating mainlyon surface geology and mineralogy; subsurface structure; and atmospheric circu-lation, composition, and long-term evolution (see Chapter 8).Regarding exobiology, the orbiter payload is able to identify signatures of water in

liquid, solid, and vapor form. In particular, the subsurface sounding radar altimeterMARSIS has delivered data to construct underground water distribution maps todepths of a few kilometers. Other Mars Express instruments continue to breakscientific ground with important discoveries. Among these are the volcanic andglacial structures observed by the high-resolution stereo camera (HRSC); the detec-tion of trace amounts ofmethane in theMartian atmosphere by the planetary Fourierspectrometer (PFS), which some scientists believe to have a biogenic origin; and theidentification of water-altered minerals by the visible and infrared mineralogicalmapping spectrometer OMEGA. A further task of Mars Express is to identify life-friendly geological regions that could become candidate landing sites for ExoMars.Regrettably, the Beagle 2 lander failed. It was meant to undertake a detailed

chemical and morphological study of its landing site and to look for water in thesoil, in rocks, and in the atmosphere. It would have sampled material fromprotected niches – subsurface and rock interiors– with a mole and a rock grind-er/corer mounted on a small robotic arm. Beagle 2 was designed to investigate theoccurrence of carbonate minerals, to determine the samples’ isotopic fractionation,and to search for trace atmospheric species.

12.1.2.1 The ESA Exobiology Science Team StudyAs a logical progression from its activities in low Earth orbit (LEO), in 1997 ESAcreated an Exobiology Science Team. Its objective was to conduct a state-of-the-art

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survey of exobiology research and to formulate recommendations for the futuresearch for life in the Solar System. The full findings were published in 1999, in theESA Special Publication ESA SP-1231, the so-called “Red Book Report.”The main recommendations were that Mars should constitute ESA’s primary

goal and that efforts should be directed mainly to the search for extinct life. Theteam identified three fundamental requirements:

• That the landing area be of high exobiological interest. Thishas not been the case in past missions. Locations rich insedimentary deposits and relatively free from wind-blowndust should be targeted.

• That samples be collected at different sites, with a rovercontaining a drill to reach well into the soil and surface rocks.This means that mobility and subsurface access are required.

• That an integral set of measurements be performed on eachsample and on the place it is obtained from.

The team suggested the following instruments for an exobiology package: a micro-scope for general examination of the samples at a resolution of 3 �m, plus a close-up camera with 50 �m resolution; an infrared or Raman spectrometer for identify-ing minerals and organic molecules; an alpha proton X-ray spectrometer (APXS)for establishing the samples’ atomic composition; a Mçssbauer spectrometer forstudying iron mineral compositions and oxidation states; a gas chromatograph–mass spectrometer (GC-MS) assembly for isotopic, organic, and inorganic molec-ular determination and for chirality measurements; and an oxidants sensor.During 1999–2000, two parallel phase-A studies were undertaken to examine the

feasibility of accommodating the instrument package proposed by the ExobiologyScience Team in a Surveyor-class lander. At the time, NASA had very ambitiousplans for the exploration of Mars, with missions to be launched every two years.ESA saw a potential for scientific cooperation through the contribution of one ormore payload elements to a future U. S. mission. The outcome of those industrialstudies was a preliminary design concept for what was called the Exobiology Multi-User Facility (EMF).

12.1.2.2 The 1999 Exobiology Announcement of OpportunityIn view of a possible collaboration with NASA, in 1999 ESA issued an Announce-ment of Opportunity (AO) requesting proposals for exobiology experiments to beperformed on Mars using the EMF. No specific flight opportunity was identified atthe time. The agency would provide the infrastructure needed for the variousinstruments: mechanical, control, power, thermal, and communications. Further,it would furnish a drill unit and a sample distribution and preparation system. Theinvestigators were to propose the scientific instruments.Sadly, the unfortunate demise of NASA’s Mars Polar Lander and Mars Climate

Orbiter put the joint-mission scenario on hold. NASA undertook a critical review ofits Mars exploration program. This resulted in a revised sequence, with fewer and

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less frequent missions than previously envisioned. All landers after the twin 2003Mars Exploration Rovers (MER) Spirit and Opportunity, dedicated to the study ofsurface mineralogy, were postponed to 2009 and beyond. In view of these events,the conditions for participating in a U. S. endeavor, as defined in the 1999exobiology AO, were no longer realistic. ESA, therefore, decided to take theinitiative in creating its own mission to search for life on Mars.

12.1.3The AURORA and the ELIPS Program of ESA

In November 2001, exobiology activities at ESA received a boost at the MinisterialConference in Edinburgh, Scotland, when the European ministers approved fund-ing for two important new programs: the exploration program AURORA and theEuropean Life and Physical Sciences in Space (ELIPS) Program. The goal of theAURORA program is to formulate and implement a European long-term plan forthe robotic and human exploration of the Solar System, particularly of those bodiesholding promise for life. The ELIPS program complements AURORA by support-ing exobiology and ISS research in LEO.To prepare for the human exploration of Mars, the AURORA programmust first

develop the necessary technologies by conducting a number of robotic missions.These missions must resolve important scientific questions connected to exobiol-ogy, planetary protection, and hazards to human missions to Mars. For the earlyexploration phase, ESA assessed a range of possible missions in cooperation withscientists. This resulted in the selection of the first two missions in the AURORAprogram:

• ExoMars: An exobiology mission for performing in situanalysis to search for traces of past and present life on Marsand to study the environment in preparation for futurehuman missions.

• Mars Sample Return (MSR): This challenging mission willreturn to Earth a small capsule carrying samples from theMartian surface. It requires a Mars orbiter, accommodatingthe Earth return and reentry capsule, and a descent module/Mars ascent vehicle. It is envisioned to implement this mis-sion in an international collaboration effort.

The approval of the AURORA and ELIPS programs signaled a strong commitmentby the member states to continue supporting exobiology research, and to ensurethe further consolidation of Europe’s role as an important partner in planetaryexploration.

12.1.3.1 The 2003 Pasteur Call for IdeasDuring 2002, at its Concurrent Design Facility, ESA carried out a study to definethe foundations for the first AURORA mission: ExoMars. This work resulted in a

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preliminary mission architecture concept and helped to estimate the level ofresources that would be available to perform surface science on the Red Planet.With that information in hand, in early 2003, ESA issued its Pasteur Call for Ideas.Scientists were invited to propose instruments for the Pasteur payload and inves-tigations to be performed with the ExoMars rover.The scientific community’s response was extremely encouraging: nearly 600

investigators from 260 universities, research institutions, and companies expressedtheir interest in participating in ExoMars. In all, 50 proposals were received. Theproposing teams consisted of international, multidisciplinary groups of investiga-tors. Thirty countries were represented, a demonstration that interest in exobiologyresearch is shared across national borders and that scientists favor internationalcollaboration. During September 2003, all instrument proposals were reviewed forscientific merit by a panel of independent experts drawn from the internationalscientific community.In March 2004, 40 scientists from the Pasteur-selected teams (representing

approximately 400 investigators) gathered at ESA/ESTEC for a full week. Theywere requested to assign priorities to the measurements needed to accuratelyidentify signs of past or present life on Mars and to characterize surface hazardsto humans. Three working groups were formed, on life detection, geologicalcontext, and environment information.On the basis of that prioritization, the science team recommended the following

science exploration scenario for ExoMars. It calls for mobility, access to the subsur-face, and research at multiple scales, starting with a visual/spectroscopic assess-ment of the geological environment around the rover, progressing to smaller-scaleinvestigations through the study of interesting surface rocks using a suite ofcontact instruments, and culminating with the collection of appropriate samplesto be analyzed by the instruments inside the rover’s laboratory.During the second half of 2004, two Rover-Pasteur phase A studies were con-

ducted in consultation with the scientists and ESA, with the goal of proposing well-integrated concepts for the Pasteur payload and the rover that would be able torealize the ExoMars science objectives. These activities were concluded in February2005.Intense discussions seeking to contain the overall mission cost in preparation for

the 2005 ESA Ministerial Conference resulted in a revised ExoMars missionconcept: a Soyuz version, carrying the rover and a small station but no orbiter.The mass allocation for the rover and Pasteur was substantially reduced from thatconsidered in the phase A studies, and a new element was introduced – thegeophysics and environment package (GEP), which could constitute a better plat-form for some of the Pasteur environment measurements.To address these payload issues, 40 scientists from the Pasteur-selected teams

gathered once again at ESA/ESTEC for the second Pasteur working group meetingduring September 2005. Also present were investigators from the GEP communityand from ESA’s advisory bodies, delegations, and NASA representatives. Theparticipants recommended a payload of 12.5 kg for the rover. They stressed thatExoMars, with its subsurface drill, would provide a unique opportunity to effec-

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tively search for life on Mars. Having reduced the rover’s instrument mass from24 kg to 12.5 kg, they underlined that the recommended payload is considered theminimum necessary to do the job properly. The meeting concluded with a strongrequest by the scientists that the proposed 12.5 kg Pasteur payload for life detectionbe implemented in its entirety onboard the rover. Equally firmly was stressed theneed to include the Pasteur environment instruments in the mission and toconfirm the implementation of the GEP station in ExoMars.

12.1.3.2 Approval of the ExoMars MissionThe ExoMars mission was approved at the ESA Ministerial Conference in Berlin,Germany, in December 2005. At the time of this writing, mid-2006, the project ishalfway through its design phase. Development of the manufacturing phase isexpected to begin in early 2008.

12.2ExoMars Science Objectives

Establishing whether life ever existed on Mars, or is still active today, is one of theoutstanding scientific questions of our time. It is also a necessary prerequisite toprepare for future human exploration endeavors. To address this important goal,ESA plans to launch the ExoMars mission.The ExoMars mission’s scientific objectives are:

• to search for signs of past and present life on Mars;• to characterize the water/geochemical environment as a

function of depth in the first 2 m of the subsurface;• to study the surface environment and identify hazards to

future human missions; and• to investigate the planet’s deep interior to better understand

Mars’s evolution and habitability.

12.2.1Searching for Signs of Life

In attempting to define an effective strategy to search for carbon-based life onMars,a useful approach is initially to ponder separately the issues of past and present lifedetection and, subsequently, to look for a common thread that may suggest a wayto address both cases.

12.2.1.1 Extinct LifeIf life ever arose on the Red Planet, it may have happened when Mars was warmerand wetter, during its initial half-billion to one billion years. Conditions then wereprobably similar to those on early Earth. Therefore, onemay reasonably expect that,

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likewise, life emerged on early Mars and that microbes quickly became a globalphenomenon. Nevertheless, there is inevitably a large measure of chance involvedin finding convincing evidence of ancient life forms.On our planet’s surface, the permanent presence of running water, atmospheric

oxygen, and life itself quickly erases all traces of any exposed, dead organisms. Theonly opportunity to detect them is to find their biosignatures encased in a protec-tive environment, i.e., in suitable rocks. However, high-temperature metamorphicprocesses and plate tectonics have resulted in the reforming of most ancientterrains, and thus it is very difficult to find rocks on Earth older than 3 billionyears in good condition. The ensuing chemical and isotopic degradation of manyputative bacterial fossils makes their reliable identification far from trivial.A further complication is that a range of inorganic processes is known to result

in mineral structures closely resembling primitive biological shapes. This issue liesat the heart of a heated debate among paleobiologists. Two recent examples thathave attracted much attention are the early Archean rock specimens (Archean isthe earliest part of the Precambrian era on Earth, approximately 3.8–2.5 billionyears ago) obtained from the Pilbara region of Western Australia, claimed tocontain Earth’s oldest fossils to date (see Chapter 1), and the Martian meteoriteALH84001, whose alleged fossil microorganisms were seen worldwide in 1996.Although resembling very small bacteria found on our planet, there is still con-siderable controversy as to the nature of these structures (see Chapter 8). Thedifficulty is that, in essence, one is looking for the exiguous remnants of minus-cule, unshelled, uncompartmentalized beings whose fossilized forms can besufficiently simple to be confused with tiny mineral precipitates. It is thereforedoubtful that the living origin of ancient candidate microfossils may be accuratelyestablished on the basis of their morphology alone. Although important, compa-rative anatomy by itself cannot be relied upon to provide sufficient proof.Another useful clue may lie in the isotopic signature of carbon. Many life

processes favor the assimilation of the light isotope, 12C, over that having an extraneutron, 13C. This gives rise to a higher concentration of 12C in living cells relativeto the one found in the surrounding dead environment. For instance, the enzy-matic uptake of carbon during photosynthesis can result in a 12C:13C ratio of about91–94, whereas the terrestrial ratio taken as standard for abiotic material is just 89.Consequently, provided that they can be isolated, carbon residues stemming frompreviously living matter may be recognized by their 12C enrichment. However, fora useful interpretation of isotope biosignatures, a detailed understanding of thesources and sinks, as well as their temporal evolution, is crucial.Some compounds synthesized by living organisms are so stable that they can last

for billions of years after the parent organisms have died and decomposed. It is notthe whole molecule that survives, but rather the backbone of carbon atoms with itsdistinctive geometry. Typical examples are amino acids, the lipids that comprisecell walls, and some pigments, such as chlorophyll, which absorbs light to powerphotosynthesis in plants. These telltale molecules are very common on our planetand can constitute very reliable biomarkers. Identifying one of them could prove asinformative as finding a dinosaur bone.

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Regrettably, a major problem with the study of biomarkers is that many decom-pose when exposed to temperatures greater than 200�C. On Earth, most Archeanrocks have been heated beyond this value. Mars, on the other hand, has notsuffered such widespread tectonic activity. Long-lasting volcanism seems to haveconcentrated mainly on large provinces, such as the Tharsis and Elysium regions.This would imply that rock formations from the earliest period of Martian history,which have not been exposed to high-temperature recycling, may exist. Conse-quently, well-preserved ancient biomarkers may still be accessible for analysis.Some of life’s most important molecular building blocks, namely, amino acids

and sugars, can exist in left- and right-handed configurations called enantiomers(from the Greek enantios, denoting “opposite” or “opposing”), which, like a pair ofgloves, are mirror images of one another (Fig. 12.1) (see also Chapter 3). On Earthall living organisms use one enantiomer only: left-handed in the case of aminoacids and right-handed for sugars. This property is called homochirality, a com-pound word derived from Greek, meaning “same handedness.” Homochirality isessential for an efficient metabolism. Key life processes, such as protein synthesisand gene transcription, rely on amino acids and sugars having the correct spatialconformation to “shake hands” at the molecular level with their counterparts.Conversely, synthetic chemicals prepared in the laboratory exhibit equal abundan-ces of both right- and left-handed enantiomers. Such a mixture is said to beracemic. Homochirality probably constitutes the most reliable indicator of thebiological versus abiotic origin of organic molecules. Surely, testing for homochir-ality becomes crucial when searching for life. However, as with the previousmethods outlined, this biosignature unfortunately will be lost when the sampleis exposed to high temperatures or wet conditions for extended periods.In summary, the best chance to find signatures of ancient life on Mars is in the

form of chemical biomarkers and fossil communities, either preserved under-ground or encased within surface rocks. A few life-detection methods – by nomeans exhaustive – were presented to illustrate how important it is to usecomplementary techniques that, combined, give more credence to the propositionof a sample’s biological potential. Several independent lines of evidence arerequired to construct a compelling case. ExoMars must therefore pursue a holisticsearch strategy, attacking the problem from multiple angles, including geological

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Fig. 12.1 Sketch demonstratingthe chirality of amino acids (imagecredit: J. L. Bada).

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and environmental investigations (to characterize potential former habitats), visualexamination of samples (morphology), and spectrochemical composition analyses.It is important to note that exposure of fossil-bearing rocks to thermal reforma-

tion greatly degrades any biogenic morphological, chemical, or isotopic signatures.Thus, geologically recent volcanic regions and lava flows should be avoided whensearching for traces of extinct life.Because liquid water is a prerequisite for active life, good candidate locations to

look for microfossils are terrains occupied by long-lasting bodies of water duringMars’s early history, e.g., within ancient lacustrine ormarine sedimentary rocks thataccumulated rapidly, where subsequent diagenesis did not obliterate the originaltexture and compositional evidence – isotopic, organic, and mineralogical – of thedeposition environment. (The term diagenesis refers to the physical and chemicalchanges occurring in sediments between the time of deposition and petrification.)Some promising sites have been identified through the analysis of images taken bythe cameras of the current spacecraft orbiting Mars, such as Mars Global Surveyor,Odyssey, and Mars Express. One such example is presented in Fig. 12.2.Figure 12.2 a shows a section of what may have been a lake in southwestern

Chandor Chasma (6.4 � S, 77.1 � W), a region within the Valles Marineris system.Figure 12.2 b is a high-resolution image, corresponding to the small, white rec-tangle in Fig. 12.2 a. It reveals that the floor at this location contains numerouseroded, layered outcrops. Particularly interesting is the large number and uni-formity of the layers or beds. They can be appreciated in more detail in Fig. 12.2 c.The thickness of the individual layers is estimated to be approximately 10 m. Theyhave smooth upper surfaces and are hard enough to form sharp, cliff-like edges,

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Fig. 12.2 Example of sedimentary outcrops onMars. (a) Liquid-carved terrain in southwesternCandor Chasma (6.4 � S, 77.1 � W); (b) high-resolution image corresponding to the smallwhite rectangle in (a); (c) detailed view of the

layers or beds whose individual height isestimated to be about 10m; (d) for compar-ison, similar features in the Grand Canyon(image credit: NASA/JPL/MalinSSS).

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which suggest that the beds may consist of indurated fine particles. (Indurationmeans the hardening or cementing process that consolidates sediments to formsedimentary rocks.) On Earth, such regular layers signal episodic interruptions inthe material deposition process. Patterns like these are usually associated withsediments accumulated in dynamic aqueous environments over very long periods,spanning several hundred million years. The similarities to terrestrial watersedimentation patterns are striking. For comparison, Fig. 12.2 d displays sedimen-tary rocky outcrops in the Grand Canyon. The layers in the foreground are knownas the Dox Formation; they were deposited in rivers and floodplains more than abillion years ago.It is trapped within old, exposed sedimentary material and evaporitic deposits

that the record of ancient Martian life, if it ever existed, is likely to be preserved.

12.2.1.2 Extant LifeIn 1976, NASA’s twin Viking landers conducted the first in situ measurementsfocusing on the detection of organic compounds and life on Mars. The Vikingbiology package contained three experiments, all looking for signs of metabolismin soil samples. One of them, the labeled-release experiment, produced veryprovocative results (see Chapter 5). If other information had not been availableas well, these data could have been interpreted as proof of biological activity.However, theoretical modeling of the Martian atmosphere and regolith chemistryhinted at the existence of powerful oxidants, which could more or less account forthe results of the three biology package experiments. The biggest blow was thefailure of the Viking gas chromatograph–mass spectrometer (GC-MS) to findevidence of organic molecules at the parts-per-billion (ppb) level. Although notintended as a life-detection experiment, the GC-MS measurements were regardedto be inconsistent with a biochemical explanation for the labeled-release data. Itmust be stressed that the Viking GC-MS was not designed to search for living cells,but rather for the gaseous pyrolytic degradation products of organic substances.Hence, this instrument could have missed significant amounts of non-volatileorganic compounds. Recent work suggests that the sensitivity of the VikingGC-MSmay have been insufficient to detect the organics released by heat from up to30 million bacteria per gram of soil. This number reflects the concentration ofmicroorganisms detected, e.g., in permafrost samples on Earth. The interpretationthat the labeled-release results may be due to the action of highly reactive oxidantsin the regolith is still debated; nevertheless, with few exceptions, the majority of thescientific community has concluded that the Viking results do not demonstrate thepresence of life.Numerous attempts have been made in the laboratory to simulate the reactions

observed by the Viking biological package. While some have reproduced certainaspects of the data, none has succeeded entirely. An oxidant experiment was part ofthe Russian Mars ’96 scientific payload. Alas, a launcher failure meant the loss ofthat opportunity to characterize the reactivity of the Martian soil. Incredibly, almost30 years after the Vikingmissions, the crucial chemical oxidant hypothesis remains

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untested. ExoMars will therefore include a powerful instrument to study oxidantsand their relation to organics distribution on Mars.Undoubtedly, the present environment on Mars is exceedingly hostile for the

widespread proliferation of surface life: it is simply too cold and dry, not to mentionthe large doses of UV radiation. Notwithstanding these hazards, basic organismsmay still flourish in protected places: deeply underground, at shallow depths inespecially benign environments, or within rock cracks and inclusions.Perhaps a good first step is to consider Earth ecosystems with conditions

approximating those of the Red Planet. In this regard, it is the frigid desert ofthe Antarctic dry valleys (77 � 45’ S) that bears the closest resemblance to theMartian environment today. This region has temperatures varying between –15 �Cand 0�C in the summer, and as low as –60�C during the winter, with a relativehumidity of 16–75%. The melting of the infrequent snow coverage on rocks is themain source of water for life there.The primary producers are photosynthetic endolithic microbial communities

dominated by cryptoendolithic lichens. These microorganisms colonize a narrowzone a few millimeters beneath the surface of rocks (Fig. 12.3). This habitatprovides a favorable microclimate and is well protected from the harsh outsideenvironment (strong winds, temperature fluctuations, desiccation, and UV radia-tion). Cryptoendolithic communities are found only in weathered or porous rocks,because only these types of rocks offer the necessary substrate to colonize theirinterior, the permeability for the uptake of liquid water and moisture, and thetranslucent property required for the photosynthetic primary producer. Usually,endoliths grow only on the faces of rocks where the highest insolation is received:in Antarctica, north-facing or horizontal. Water is provided to the rock by blowingsnow or frost, which melts into the rock when it is warmed by sunlight. During thesummer, freeze–thaw transitions are common. The endoliths are wetted either byequilibration with the high-humidity air in the rock or by direct moisture uptakeafter snow/frost melt.A similar kind of microhabitat could be available on Mars. From the Viking

mission we know that surface frost is widespread in the morning hours at certainlocations; in addition, the Pathfinder landing site contained many weathered rocks.Cryptoendolithic communities colonizing the interstitial space in Martian rockswould be protected from the harsh UV radiation. Even after the extinction of these

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Fig. 12.3 Cryptoendolithic microorganismsfrom the McMurdo Dry Valleys, Antarctica.These cold-adapted communities live in favor-able microclimates, just beneath the surfaceof porous rocks facing the Sun (image credit:Russ Kinne, NSF).

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communities, certain stable biomarkers, such as pigments, might be preserved inthe cold and dry environment for long periods. Life could have escaped thedeteriorating climatic conditions on the surface of Mars by finding refuge inhabitats that are very similar to those colonized by cryptoendolithic communitiesin Antarctica. Finding out whether this happened will be part of the investigationsperformed by the ExoMars mission.

12.2.1.3 Search for Life: ConclusionsThe strategy to find traces of past biological activity rests on the assumption thatany surviving signatures of interest will be preserved in the geological record, in theform of buried/encased remains, organic materials, and fossil communities.Similarly, because current Martian surface conditions are hostile to most knownorganisms, also when looking for signs of extant life, the search methodologyshould focus on investigations in protected niches: underground, in permafrost, orwithin surface rocks. Therefore, the same sampling device and instrumentationcan adequately serve both types of studies. The biggest difference is due to locationrequirements. When searching for extinct life, the interest lies in areas occupied byancient bodies of water over many thousands of years. For extant life, the emphasisis on water-rich environments close to the surface and accessible to our sensorstoday. For the latter, the presence of permafrost alone may not be enough.Permafrost in combination with a sustained heat source, probably of volcanic orhydrothermal origin, may be necessary. Such warm oases can only be identified byan orbital survey of the planet. In the next few years, a number of remote sensingsatellites, such as ESA’s Mars Express and NASA’s Mars Reconnaissance Orbiter(MRO), will determine the water–ice boundary across Mars and may help todiscover any such warm spots. If they do exist, they would be prime targets formissions such as ExoMars.On Earth, microbial life quickly became a global phenomenon. If the same

explosive process occurred on the young Mars, the chances of finding evidence ofpast life may be good. Even more interesting would be the discovery and study oflife forms that have successfully adapted to modern Mars, such as the cryptoendo-lithic communities discussed in Section 12.2.1.2. However, this presupposes theprior identification of geologically suitable, life-friendly locations where it can bedemonstrated that liquid water still exists, at least episodically throughout the year.For these reasons, the “Red Book” science team advised ESA to focus mainly on thedetection of extinct life, but also to build enough flexibility into the mission designto be able to target sites with potential for present life.

12.2.2Hazards for Human Operations on Mars

Before astronauts can be sent to Mars, one must understand and control any risksthat may pose a threat to a mission’s success. Some of these risks will be assessedwith ExoMars.

12 Putting Together an Exobiology Mission: The ExoMars Example334

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Ionizing radiation is probably the single most important limiting factor forhuman interplanetary flight. To evaluate its danger and to define efficient miti-gation strategies, it is desirable to incorporate radiation-monitoring capabilitiesduring cruise, orbit, and surface operations on precursor robotic missions to Mars.Another physical hazard may result from the basic mechanical properties of the

Martian soil. Dust particles will invade the interior of a spacecraft during surfaceoperations, as shown by the Apollomissions to the Moon. Dust can pose a threat toastronauts on Mars, and even more so under microgravity during the return flightto Earth. Characteristics of the soil, such as the size, shape, and composition ofindividual particles, can be studied with dedicated in situ instrumentation. How-ever, a more in-depth assessment, including a toxicity analysis, will require thereturn of a suitable Martian sample.Reactive inorganic substances could constitute chemical hazards on the Martian

surface. Free radicals, salts, and oxidants are very aggressive in the presence ofhumidity, e.g., in the lungs and eyes. In addition, toxic metals, organics, andpathogens are potential hazards. As with dust, chemical hazards present in thesoil might contaminate the interior of a spacecraft during surface operations. Theycould affect the health of astronauts and the operation of equipment. Manypotential inorganic and organic chemical hazards may be identified with theExoMars search-for-life instruments.

12.2.3Geophysics Measurements

The processes that have determined the long-term habitability of Mars depend onthe geodynamics of the planet and on its geological evolution and activity. Im-portant issues still need to be resolved: What is Mars’s internal structure? Is thereany volcanic activity on Mars? The answers may allow us to extrapolate into thepast, to estimate when and how Mars lost its magnetic field and the importance ofvolcanic outgassing for the early atmosphere.ExoMars will carry a geophysics and environment package (GEP), accommo-

dated on the descent module.

12.3ExoMars Science Strategy

The mission strategy to achieve the scientific objectives of ExoMars is as follows:• To land on, or be able to reach, a location of high exobiology

interest for past and/or present life signatures, i.e., access tothe appropriate geological environment.

• To collect scientific samples from different sites, using a rovercarrying a drill system capable of reaching well into the soiland surface rocks. This requires mobility and access to thesubsurface.

12.3 ExoMars Science Strategy 335

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• To conduct at each site an integral set of measurementsat multiple scales (Fig. 12.4), beginning with a panoramicassessment of the geological environment, progressing tosmaller-scale investigations on interesting surface rocksusing a suite of contact instruments, and culminating withthe collection of well-selected samples to be studied by therover’s analytical laboratory.

• To characterize the environment and the geophysical pa-rameters relevant for life, the hazards to humans, and theplanetary evolution.

To arrive at a clear and unambiguous conclusion on the existence of past or presentlife at rover sites, it is essential that the search instrumentation be able to providemutually reinforcing lines of evidence, while minimizing the opportunities foralternative interpretations. It is imperative that all instruments be carefully de-signed so that none becomes a weak link in the chain of observations. Performancelimitations in an instrument intended to confirm the results obtained by anothershould not generate confusion and discredit the whole measurement.

12 Putting Together an Exobiology Mission: The ExoMars Example336

Fig. 12.4 The ExoMars surface science ex-ploration scenario. The rover will conductmeasurements at multiple scales, starting witha panoramic assessment of the geologicalenvironment, progressing to smaller-scale in-

vestigations on interesting surface rocks usinga suite of contact instruments, and culminatingwith the collection of well-selected samples tobe studied by the rover’s analytical laboratory(image credit: ESA).

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The science strategy for the Pasteur payload is therefore to provide a self-consistent set of instruments that can obtain reliable evidence for or against theexistence of a range of biosignatures at each search location. This will be achievedthrough the detection of organic compounds and oxidants, as well as by determin-ing the geological context, mineralogy, and geochemistry of the samples beinganalyzed.

12.4ExoMars Mission Description

The baseline mission scenario, shown in Fig. 12.5, consists of a spacecraft compo-site with a carrier and a descent module, launched by a Soyuz 2 b rocket fromKourou, Europe’s spaceport in French Guiana. It will follow a two-year “delayedtrajectory” designed to reach Mars after the statistical dust storm season. Thecarrier will release the descent module from the hyperbolic arrival path. Thedescent module will enter the Martian atmosphere, land (using either bouncing[non-vented, as in MER] or non-bouncing [vented] airbags), and deploy the roverand GEP. In the baseline mission, data relay for the rover will be provided by aNASA orbiter. The main characteristics of the ExoMars mission are listed inTable 12.1.

12.4 ExoMars Mission Description 337

Fig. 12.5 The ExoMars “baseline” mission architecture, based ona “carrier plus descent module” composite launched by a Soyuz2 b rocket. The descent module is released from the hyperbolicarrival trajectory and delivers the rover to the Martian surface(image credit: ESA).

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Table 12.1 Main characteristics of the ExoMars mission.

Area Type Specification

Technical data Spacecraft Carrier plus descent module including roverand GEP[c]

Data relay provided by NASALaunch May–June 2013, from Kourou on Soyuz 2 b

(backup 2015)Arrival at Mars June 2015 (backup 2017)Landing on Mars Direct entry, from hyperbolic trajectory, after the

dust storm season.Latitudes between 15º S and 45º N, all longitudes;Altitude: £ 0m, relative to the MGS/MOLA[a]

zero levelScience Rover + Pasteur Mass 170–190 kg, includes drill system, SPDS[b],

and instruments (8 kg);Lifetime ‡ 180 sols

GEP[c] Mass £ 20 kg; includes instruments (4–5 kg);Lifetime ‡ 1 year

Ground segment Missioncontrol/missionoperations

European Space Observation Center (Germany)

Rover operationon Mars surface

Rover Operations Center (Italy)

GEP[c] operations To be decided

a Mars Global Surveyor/Mars Orbiter Laser Altimeterb Sample preparation and distribution systemc Geophysics and environment package

An alternative configuration, based on an Ariane 5 ECA launcher, may be imple-mented depending on programmatic, technical, and financial considerations(Ariane 5 ECA is the latest version of the Ariane 5 launcher. In this option (Fig.12.6), the carrier is replaced by an orbiter that provides end-to-end data relay for thesurface elements. The orbiter will also carry a science payload to complement theresults from the rover and the GEP and provide continuity to the great scientificdiscoveries of Mars Express.ExoMars is a search-for-life mission targeting regions with high life potential. It

has therefore been classified as planetary protection category IVb/c (see Chapter13). This, coupled with the mission’s ambitious scientific goals, imposes challeng-ing requirements regarding sterilization and organic cleanliness.

12 Putting Together an Exobiology Mission: The ExoMars Example338

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12.4.1The ExoMars Rover

The ExoMars rover will have a nominal lifetime of 180 sols (approximately6 months, 1 sol = 24 h and 39 min). During this period, it will ensure a regionalmobility of several kilometers, relying on solar array electrical power (Fig. 12.7).The Pasteur model payload (see Tables 12.2 and 12.3) contains:

• panoramic instruments (cameras, a ground-penetratingradar, and an IR spectrometer);

• contact instruments for studying surface rocks and soils(close-up imager and Mçssbauer spectrometer);

• a subsurface drill capable of reaching depths down to 2 m andof collecting specimens from exposed bedrock;

• a sample preparation and distribution system; and• the analytical laboratory.

The latter includes a microscope, an oxidation sensor, and a variety of instrumentsfor characterizing the organic substances and the geochemistry in the collectedsamples.

12.4 ExoMars Mission Description 339

Fig. 12.6 The ExoMars “orbiter” option architecture, based onan “orbiter plus descent module” composite launched by anAriane 5 ECA rocket. The descent module delivers the rover tothe Martian surface, and the orbiter includes a science payload(image credit: ESA).

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12 Putting Together an Exobiology Mission: The ExoMars Example340

Table12

.2Recom

men

dedPa

steu

rexob

iology

instrumen

ts.

Instrumen

tFu

nctio

n

Pan

oram

icinstrumen

tsTocharacterize

therover’sgeolog

ical

environmen

t,bo

thon

thesurfacean

din

thesubsurface.

Typical

scales

span

from

kilometersto

meters,withsub-centimeter

resolution

forclosetargets.

Pan

oram

iccamerasystem

Twowide-an

glestereo

cameras

pluson

ehigh-resolution

camera;to

characterize

therover’sgeolog

ical

environmen

t.Veryim

portan

tforscientifictarget

selection.

Infrared

(IR)spectrom

eter

For

theremoteiden

tification

ofwater-related

mineralsan

dforscientifictarget

selection.

Groundpenetratingradar

Toestablishthesubsurfacestratigraphydo

wnto

3-m

depthan

dto

helpplan

thedrillingstrategy.

Con

tact

instrumen

tsToinvestigatesurfacerocksan

dsoils.A

mon

gthescientificinterestsatthisscalearemacroscop

ictextures,structures,

andlayeringan

dbu

lkmineralog

ical

andelem

entalcontent.Thisinform

ationwill

befundamen

talforcollecting

samples

formoredetaile

dan

alysis.T

hepreferredsolution

isto

deploy

thecontactinstrumen

tsusingan

arm-and-paw

arrangemen

t,as

inBeagle2.Alternatively,in

case

ofmasslim

itations,they

could

beaccommod

ated

atthebase

ofthe

subsurfacedrill.

Close-upim

ager

Tovisually

investigatescientifictargetsat

thecentimeter

range

withsub-millim

eter

resolution

.

Mçssbau

erspectrom

eter

Tostudy

themineralog

yof

Fe-bearingrocksan

dsoils.

Ram

an-LIB

S[a]external

opticalheads

Todeterm

inethegeochem

istryof

rocksan

dsoils.T

heseareexternal

heads

connectedto

theinstrumen

tsinside

the

analytical

labo

ratory.

Facility-supp

ortequipmen

tTheseessential

system

saredevotedto

theacqu

isitionan

dpreparationof

samples

fordetaile

dinvestigationsin

the

analyticallabo

ratory.T

hey

mustfollo

wspecificacqu

isitionan

dpreparationprotocolsto

guaran

teetheop

timalsurvival

ofan

yorganicmoleculesan

dvolatilesin

thesamples.T

hemission

’sabilityto

breaknew

scientificgrou

nd,particularly

forsign

s-of-life

investigations,depends

onthesetw

oinstrumen

ts.

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12.4 ExoMars Mission Description 341

Instrumen

tFu

nctio

n

Subsurfacedrill

Capableof

obtainingsamples

from

0to

2m

depth,w

hereorganicmoleculesan

dvolatilesmightbe

wellp

reserved.It

also

integrates

temperature

sensors

andan

IRspectrom

eter

forbo

reholemineralog

ystudies.

SPDS[

b]Receivesasamplefrom

thedrill

system

,preparesitforscientifican

alysis,andpresen

tsitto

allan

alytical

labo

ratory

instrumen

ts.A

very

impo

rtan

tfunctionisto

prod

uce

particulate

materialwhile

preservingtheorganic

andwater

content.

Analytical

labo

ratory

Tocondu

ctadetaile

dan

alysisof

each

collected

sample.Thefirststep

isavisual

andspectroscopicinspection

.Ifthe

sampleisdeem

edinteresting,

itisgrou

ndupan

dtheresultingparticulate

materialisusedto

search

fororganic

moleculesan

dto

perform

more-accurate

mineralog

ical

investigations.

Microscop

e(VIS

+IR

)Toexam

inethecollected

samples

tocharacterize

theirstructure

andcompo

sition

atthegrain-sizelevel.These

measuremen

tswill

also

beusedto

select

samplelocation

sforfurther

detaile

dan

alyses

bytheRam

an-LIB

Sspectrom

eters.

Ram

an-LIB

STodeterm

inethegeochem

istryof

thecollected

samples.

X-ray

diffractom

eter

Todeterm

inethetruemineralog

ical

compo

sition

ofasample’scrystallineph

ases.

Urey

(MarsOrgan

ics+OxidantDetector)

TheMarsOrgan

icsDetectorsearches

foram

inoacids,nucleobases,an

dpo

lyarom

atichydrocarbon

sin

thecollected

samples

withextrem

elyhighsensitivity

(ppt).Can

also

functionas

fron

t-en

dto

theGC-M

S.T

heMarsOxidant

Instrumen

tdeterm

ines

thechem

ical

reactivity

ofoxidan

tsan

dfree

radicalsin

thesoilan

datmosph

ere.

GC-M

STocondu

ctabroad-range,veryhigh-sen

sitivity

search

fororganic

moleculesin

thecollected

samples;a

lsofor

atmosph

eric

analyses.

Life-M

arkerChip

Antibo

dy-based

instrumen

tto

detect

organic

moleculeswithvery

highspecificity.

Mass(w

ithou

tdrill

andSPDS):1

2.5kg

.aLIBS:

laser-indu

cedbreakd

ownspectroscopy.

bSPDS:

samplepreparationan

ddistribu

tion

system

.

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Table 12.3 Recommended Pasteur environment instruments.

Instrument Function

Environment instruments To characterize possible hazards to future human missionsand to increase our knowledge of the Martian environment.

Dust suite Determines the dust grain size distribution and depositionrate. It also measures water vapor with high precision.

UV spectrometer Measures the UV radiation spectrum.Ionizing radiation Measures the ionizing radiation dose reaching the surface

due to cosmic rays and solar particle events.Meteorological package Measures pressure, temperature, wind speed and direction,

and sound.

Mass: 1.9 kg.

A key rover element is the drill. The reason for the 2-m requirement is the need toobtain pristine sample material for analysis. The tenuous atmosphere of Marsallows damaging space radiation to penetrate into the uppermost meters of theplanet’s subsurface, affecting the long-term preservation of organic molecules thatmight be associated with extinct life or meteoritic infall. Figure 12.8 shows thesurviving fraction of amino acids versus depth after simulated exposures of 0.5, 1,and 3 billion years to ionizing radiation in the Martian subsurface. With thepresent detection limit of 0.01 ppb per amino acid, reductions of up to 10–6 canbe tolerated (dashed line in Fig. 12.8), beyond which amino acid signatures becomeundetectable. This result indicates that when one is searching for biomarkers ofMartian life that became extinct more than 3 billion years ago, it is necessary toaccess the subsurface in the range of 2 m.On Mars, any exposed organic biomarker or life form is readily degraded by UV

radiation and by reactive oxidant species resulting from surface UV-induced

12 Putting Together an Exobiology Mission: The ExoMars Example342

Fig. 12.7 Artist’s representation of the ExoMars rover’s egressfrom the descent module (image credit: ESA).

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photochemistry. Although no clear proof regarding the presence of reactiveoxidants has yet been established, radiochemical models of the Martian atmos-phere and measurements from the Viking experiments suggest their presence onthe Martian surface. Depending on the modeling parameters, the calculated rangefor the oxidant extinction depth (i.e., the depth at which the modeled concen-tration of the oxidizing agents approaches zero because of their interaction withthe subsurface environment) is between centimeters and several meters. However,these estimates refer to global mean values. The actual penetration of putativeoxidants will depend on local conditions, such as soil/rock porosity, which canlimit their diffusion. To minimize the effects of oxidants, the ExoMars drill mustbe able to penetrate and obtain samples from well-consolidated (hard) formations,such as sedimentary rocks and evaporitic deposits, at depths beyond 1.5 m.Additionally, it is essential to avoid loose dust deposits distributed by eoliantransport. While driven by the wind, this material was intensely processed byUV radiation, ionizing radiation, and potential oxidants in the atmosphere and onthe surface of Mars. Any organic biomarkers will be highly degraded in thesesamples.The ExoMars rover must monitor and control torque, thrust, penetration depth,

and temperature at the drill bit. Grain-to-grain friction in a continuous rotary drillcan generate a heat wave in the sample, destroying the organic molecules thatExoMars seeks to detect. The drill therefore has a variable cutting protocol that candissipate heat in a science-safe manner. The drill’s full 2-m extension is achieved byassembling four sections: one drill tool rod, with an internal shutter and sampling

12.4 ExoMars Mission Description 343

Fig. 12.8 Surviving fraction of amino acidsversus depth in the Martian subsurface aftersimulated exposures of 0.5, 1, or 3 billion yearsto ionizing radiation. The dashed line at asurvival rate of 10–6 gives the present detectionlimit of 0.01 ppb per amino acid, beyond which

amino acid signatures become undetectable.Therefore, when searching for biomarkers ofMartian life that became extinct more than3 billion years ago, it is necessary to access thesubsurface in the range of 2 m. Adapted fromKminek and Bada (2006).

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collection capability, plus three extension rods (Fig. 12.9). The drill is also equippedwith an IR spectrometer for mineralogy studies inside the borehole.The analysis sequence within Pasteur’s analytical laboratory is presented in

Fig. 12.10. The drill system delivers the acquired sample to the sample preparationand distribution system (SPDS). A detailed optical/spectral inspection is per-formed using the microscope, the Raman spectrometer, and the laser-inducedbreakdown spectrometer. After these data have been studied, the rover controlcenter instructs the SPDS to grind the sample. Powder material is then distributedto the remaining instruments. The X-ray diffractometer determines the sample’smineralogy. The Mars Oxidant Instrument characterizes chemical species in theMartian soil and measures their reactivity. The Mars Organics Detector searchesfor trace levels of specific organic molecules, such as amino acids, nucleotides, andpolycyclic aromatic hydrocarbons with unprecedented sensitivity (a factor of 104

greater than the Viking GC-MS package; see Section 12.2.1.2). The GC-MS con-ducts a broad search for organic molecules. Finally, the Life-Marker Chip looks forbiomarkers using recombinant antibody technology.If any organic compounds are detected on Mars, it should be possible to

demonstrate that they were not brought from Earth. The only way to reliably provethat the rover is free from contaminants is to perform an initial measurement runusing a blank sample. It is not sufficient to do this at the instrument level, as thecontamination could still come from the sampling device. For this reason, theExoMars rover will carry three blank calibration samples that are accessible to thedrill system. Upon landing, one of the first scientific actions will be to use the drillto collect and pass a blank sample to the analytical laboratory and perform a fullinvestigation. The result of this investigation should indicate “no life” and “noorganics.” Failure to obtain this first negative reading may invalidate any latersearch-for-life findings. The second blank sample serves a different purpose. It

12 Putting Together an Exobiology Mission: The ExoMars Example344

Fig. 12.9 Artist’s view of the ExoMars rover withthe drill obtaining a sample from the Martiansubsurface (image credit: ESA).

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provides a means to directly assess the impact of sample cross-contamination. Incase organics are detected, a blank sample can be introduced into the measuringchain to quantify in situ how much the organic levels drop from those measuredusing material from the previous sample. The third blank sample is a reserve.

12.5Outlook and Conclusions

NASA’s highly successful twin MERmissions were conceived as robotic geologists.They have demonstrated the past existence of long-lasting, wet environments onMars. Their results have persuaded the scientific community that mobility is amust-have requirement for all future surface missions. Recent discoveries fromMars Express have revealed multiple deposits containing salt and clay minerals thatcan form only in the presence of liquid water. This reinforces the hypothesis thatancient Mars may have been wetter, and possibly warmer, than it is today. NASA’s2009Mars Science Laboratory will study surface geology and organics, with the goal

12.5 Outlook and Conclusions 345

Fig. 12.10 Analysis sequence within Pasteur’s analyticallaboratory (image credit: ESA).

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of identifying habitable environments. ESA’s 2013 ExoMars is the next logical step.It will have instruments to investigate whether life ever arose on the Red Planet. Itwill also be the first mission combining mobility and access to subsurface locationswhere organic molecules may be well-preserved, thus allowing for the first time aninvestigation of Mars’s third dimension: depth. This alone is a guarantee that themission will break new scientific ground. Finally, the many technologies developedfor this project will allow ESA to prepare for international collaboration on futuremissions, such as Mars Sample Return.

12.6Further Reading

12.6.1Books and Articles in Books

Brack, A, Fitton, B., Raulin, F. (Scientific Coor-dinators) Exobiology in the Solar System & TheSearch for Life on Mars, Report from the ESAExobiology Team Study 1997–1998, WilsonA. (Ed.), SP-1231, ESA Publications Division,ESTEC, Noordwijk, The Netherlands, 1999.

Godwin, R., Viking ’75 Report, in: Mars – TheNASA Mission Reports, Apogee Books, Bur-lington, Ontario, 2000.

Tokano, T. (Ed.) Water on Mars and Life,Springer, Berlin, Heidelberg, 2005.

Walter, M. (Ed.) The Search for Life on Mars,Perseus Books, Cambridge, Massachusetts,1999

Wilson, A. (Ed.) Mars Express – The ScientificPayload, ESA SP-1240, ESA PublicationsDivision, ESTEC, Noordwijk, The Nether-lands, 2004.

12 Putting Together an Exobiology Mission: The ExoMars Example346

12.6.2Articles in Journals

Allwood, A. C., Walter, M. R., Kamber, B. S.,Marshall, C. P., Burch, I.W. Stromatolitereef from the early archaen era of Australia,Nature 2006, 441, 714–718, doi:10.1038/na-ture04764.

Anderson, R. C., Dohm, J. M., Golombek,M. P., Haldemann, A.F.C., Franklin, B. J.,Tanaka, K. L., Lias, J., Peer, B. Primary cen-ters and secondary concentrations of tec-tonic activity through time in the westernhemisphere of Mars, J. Geophys. Res. 2001,106(E9), 20563–20585.

Bada, J. L., Sephton, M. A., Ehrenfreund, P.,Mathies, R. A., Skelley, A.M., Grunthaner,F. J., Zent, A. P., Quinn, R. C., Josset, J.-L.,Robert, F., Botta, O., Glavin, D. P. Life onMars: New strategies to detect life on Mars,Astron. Geophys. 2005, 46(6), 26–27,doi:10.1111/j.1468–4004.2005.46626.x.

Baker, V. R. Icy Martian misteries, Nature2003, 426, 779–780.

Baker, V. R. Water and the Martian landscape,Nature 2001, 412, 228–236.

Bell III, J. F., McSween, H. Y., Jr., Crisp, J. A.,Morris, R. V., Murchie, S. L., Bridges, N. T.,Johnson, J. R., Britt, D. T., Golombek, M. P.,Moore, H. J., Ghosh, A., Bishop, J. L., An-derson, R. C., Br�ckner, J., Economou, T.,Greenwood, J. P., Gunnlaugsson, H. P.,Hargraves, R.M., Hviid, S., Knudsen, J. M.,Madsen, M. B., Reid, R., Rieder, R., Soder-blom, L. Mineralogic and compositionalproperties of Martian soil and dust: Resultsfrom Mars Pathfinder, J. Geophys. Res. 2000,105(E1), 1721–1755.

Bell, J. Tip of theMartian iceberg? Science 2002,297, 60–61.

Bibring, J.-P., Langevin, Y., Mustard, J. F.,Poulet, F., Arvidson, R., Gendrin, A., Gon-det, B., Mangold, N., Pinet, P., Forget, F.,and the OMEGA team. Global mineralogicaland aqueous Mars history derived from

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OMEGA/Mars Express data, an ESA studyfor the search for life on Mars, Science 2006,312. 5772, 400–404, doi:10.1126/sci-ence.1122659.

Biemann, K., Oro, J., Toulmin III, P., Orgel,L. E., Nier, A.O., Anderson, D.M., Sim-monds, P. G., Flory, D., Diaz, A. V., Rush-neck, D. R., Billier, J. E., Lafleur, A. L. Thesearch for organic substances and inorganicvolatile compounds in the surface of Mars,J. Geophys. Res. 1977, 82, 4641–4658.

Boynton, W. V. Feldman, W. C., Squyres,S.W., Prettyman, T., Br�ckner, J., Evans,L. G., Reedy, R. C., Starr, R., Arnold, J. R.,Drake, D.M., Englert, P. A. J., Metzger,A. E., Mitrofanov, I., Trombka, J. I., d’Uston,C., W�nke, H., Gasnault, O., Hamara, D. K.,Janes, D.M., Marcialis, R. L., Maurice, S.,Mikheeva, I., Taylor, G. J., Tokar, R., Shino-hara, C. Distribution of hydrogen in the nearsurface of Mars: Evidence for subsurface icedeposits, Science 2002, 297, 81–85.

Brack, A., Clancy, P., Fitton, B., Hofmann, B.,Horneck, G., Kurat, G., Maxwell, J., Ori,G. G., Pillinger, C., Raulin, F., Thomas, N.,Westall, F. An Integrated Exobiology Pack-age for the search for life on Mars, Adv.Space Res. 1999, 23(2), 301–308.

Carr, M.H., Head, J. W.III. Oceans on Mars:An assessment of the observational evidenceand possible fate, J. Geophys. Res. 2003,108(E5), 5042, doi:10.1029/2002JE001963.

Carr, M.H., Malin, M. C. Meter-Scale charac-teristics of Martian channels and valleys,Icarus 2000, 146, 366–386.

Clark, B. C. Surviving the limits to life at theMartian surface, J. Geophys. Res. 1978,103(E12), 28545–28555.

Cockell, C. S. Catling, D. C., Davis, W. L.,Snook, K., Kepner, R. L., Lee, P., McKay,C. P. The ultraviolet environment of Mars:Biological implications past, present, andfuture, Planet. Space Sci. 2000, 48, 343–359.

Cockell, C. S., Raven, J. A. Zones of photosyn-thetic potential on Mars and the early Earth,Icarus 2004, 169, 300–310.

Craddock, R. A., A. D. Howard, A. D. Thecase for rainfall on a warm, wet early Mars,J. Geophys. Res. 2002, 107(E11), 5111,doi:10.1029/2001JE001505.

Dohm, J. M., Anderson, R. C., Baker, V. R.,Ferris, J. C., Hare, T.M., Strom, R. G., Rudd,L. P., Rice, J.W. Jr., Casavant, R. R., Scott,

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Edwards, H. G.M., Moody, C. D., Jorge Villar,S. E., Wynn-Williams, D. D. Raman spec-troscopic detection of key biomarkers of cy-anobacteria and lichen symbiosis in extremeAntarctic habitats: Evaluations for Marslander missions, Icarus 2005, 174, 560–571,doi:10.1016/j.icarus.2004.07.029.

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Haberle, R.M., McKay, C. P., Schaeffer, J.,Cabrol, N. A., Grin, E. A., Zent, A. P.,Quinn, R. On the possibility of liquid wateron present-day Mars, J. Geophys. Res. 2001,106, E10, 23317–23326.

Hartmann,W.K., Thorsteinsson, T., Sigurds-son, F. Martian hillside gullies and Icelandicanalogues, Icarus 2002, 162, 259–277.

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Head, J. W., Neukum, G., Jaumann, R., Hie-singer, H., Hauber, E., Carr, M., Masson, P.,Foing, B., Hoffmann, H., Kreslavsky, M.,Werner, S., Milkovich, S., van Gasselt, S.,and The HRSC Co-Investigator Team.Tropical to mid-latitude snow and iceaccumulation, flow and glaciation on Mars,Nature 2005, 434, 346–351, doi:10.1038/nature03359.

Head, J. W., G. Neukum, G., Jaumann, R.,Hiesinger, H., Hauber, E., Carr, M., Mas-son, P., Foing, B., Hoffmann, H., Kreslav-sky, M., Werner, S., Milkovich, S., van Gas-selt, S., and The HRSC Co-InvestigatorTeam. Planetary science: Are there activeglaciers on Mars? (Reply), Nature 2005, 438,E10, doi:10.1038/nature04358.

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Greeley, R., Grotzinger, J., Hayes, A. G.,Hviid, S. F., Johnson, J. R., Joliff, B., Kinch,K.M., Knoll, A. H., Madsen, M. B., Maki,J. N., McLennan, S. M., McSween, H. Y.,Ming, D.W., Rice, J. W., Jr., Richter, L.,Sims, M., Smith, P. H., Soderblom, L. A.,Spanovich, N., Sullivan, R., Thompson, S.,Wdowiak, T., Weitz, C., Whelley, P. Evi-dence from Opportunity’s Microscopic Im-ager for water on Meridiani Planum, Science2004, 306, 1727–1730.

Horneck, G. The microbial world and thecase for Mars, Planet. Space Sci. 2000, 48,1053–1063.

Jakosky, B.M., Phillips, R. J. Mars’ volatile andclimate history, Nature 2001, 412, 237–244.

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Kargel, J. S. Proof for water, hints for life?Science 2004, 306, 1689–1691.

Klein, H. P. The search for life on Mars: Whatwe learned from Viking, J. Geophys. Res.1978, 103(E12), 28463–28466.

Klein, H. P. The Viking biological experimentson Mars, Icarus 1978, 34, 666–674.

Kminek, G., Bada, J. L., Botta, O., Glavin, D. P.,Grunthaner, F. MOD: An organic detectorfor the future robotic exploration of Mars,Planet. Space Sci. 2000, 48, 1087–1091.

Kminek, G., Bada, J. L. The effect of ionisingradiation on the preservation of amino acidsonMars,Earth Planet. Sci. Lett. 2006, 245, 1–5.

Komatsu, G., Ori, G. G. Exobiological implica-tions of potential sedimentary deposits onMars, Planet. Space Sci. 2000, 48, 1043–1052.

Krasnapolsky, V. A. Some problems related tothe origin of methane on Mars, Icarus 2006,180, 359–367, doi:10.1016/j.icarus.2005.10.015.

Lepland, A., van Zuilen, M. A., Arrhenius, G.,Whitehouse, M. J., Fedo, C.M. Questioningthe evidence for Earth’s earliest life–Akiliarevisited, Geology 2005, 33, 1, 77–79,doi:10.1130/G20890.1.

Leovy, C. Weather and climate on Mars,Nature2001, 412, 245–249.

Magnani, P. C., Ylikorpi, T., Cherubini, G.,Olivieri, A. Deep Drill (DeeDri) for Marsapplication, Planet. Space Sci. 2004, 52,79–82, doi:10.1016/j.pss.2003.08.023.

Mahaney, W. C., Dohm, J. M., Baker, V. R.,Newsom, H. E., Malloch, D., Hancock,

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R. G. V., Campbell, I., Sheppard, D., Milner,M.W., Morphogenesis of Antarctic paleo-sols: Martian analogue, Icarus 2001, 154,113–130.

Malin, M. C., Carr, M.H. Groundwater for-mation of Martian valleys, Nature 1999, 397,589–591.

Malin M. C., Edgett, K. S. Sedimentary rocks ofearly Mars, Science 2000, 290, 1927–1937.

Mangold, N., Quantin, C., Ansan, V., Dela-court, C., Allemand, P. Evidence for precip-itation on Mars from dendritic valleys in theValles Marineris area, Science 2004, 305,78–81.

Mars, M., Malin, C., Edgett, K. S. Evidence forpersistent flow and aqueous sedimentationon early Mars, Science 2003, 302, 1931–1934.

McKay, D. S., Gibson, E. K. Jr., Thomas-Keprta,K. L., Vali, H., Romanek, C. S., Clemmett,S. J. Chillier, X. D. F., Maechling, C. R.,Zare, R. N. Search for past life on Mars:Posible relic biogenic activity in Martianmeteorite ALH84001, Science 1996, 273,924–930.

Milliken, R. E., Mustard, J. F., Goldsby, D. L.Viscous flow features on the surface ofMars: Observations from high-resolutionMars Orbiter Camera (MOC) images,J. Geophys. Res. 2003, 108(E6), 5057,doi:10.1029/2002JE002005.

Mitrofanov, I., Anfimov, D., Kozyrev, A., Lit-vak, M., Sanin, A., Tret’yakov, V., Krylov, A.,Shvetsov, V., Boynton, W., Shinohara, C.,Hamara, D., Saunders, R. S. Maps of sub-surface hydrogen from the High-EnergyNeutron Detector, Mars Odyssey, Science2002, 297, 78–81.

Moore, J. M., Howard, A. D. Large alluvial fanson Mars, J. Geophys. Res. 2005, 110, E04005,doi:10.1029/2004JE002352.

Mustard, J. F. A wet and altered Mars, Nature2002, 417, 234–235.

Neukum, G., Jaumann, R., Hoffmann, H.,Hauber, E., Head, J. W., Basilevsky, A. T.,Ivanov, B. A., Werner, S. C., van Gasselt, S.,Murray, J. B., McCord, T., and The HRSCCo-Investigator Team. Recent and episodicvolcanic and glacial activity on Mars revealedby the High Resolution Stereo Camera,Nature 2004, 432, 971–979, doi:10.1038/nature03231.

Ori, G. G., Marinangeli, L., Komatsu, G., Mar-tian paleolacustrine environments and their

geological constrains on drilling operationsfor exobiological research, Planet. Space Sci.2000, 48, 1043–1052.

Patel, M. R., B�rces, A., Kolb, C., Lammer, H.,Rettberg, P., Zarnecki, J. C., Selsis, F. Sea-sonal and diurnal variation in Martian sur-face UV irradiation: Biological and chemicalimplications for the Martian regolith, Int.J. Astrobio. 2003, 2(1), 21–34.

Piccardi, G., Plaut, J. J., Biccari, D., Bombaci,O., Calabrese, D., Cartacci, M., Cicchetti, A.,Clifford, S.M., Edenhofer, P., Farrel, W.M.,Federico, C., Frigeri, A., Gurnett, D. A.,Hagfors, T., Heggy, E., Herique, A., Huff,R. L., Ivanov, A. B., Johnson, W. T. K., Jor-dan, R. L., Kirchner, D. L., Kofman, W.,Leuschen, C. J., Nielsen, E., Orosei, R.,Pettinelli, E., Phillips, R. J., Plettemeier, D.,Safaeinili, A., Seu, R., Stofan, E. R., Van-naroni, G., Watters, T. R., Zampolini, E.Radar soundings of the subsurface of Mars,Science 2005, 310, 1925–1928.

Pondrelli, M., Baliva, A., Di Lorenzo, S., Mari-nangeli, L., Rossi, A. P. Complex evolutionof paleolacustrine systems on Mars: An ex-ample from the Holden Crater J. Geophys.Res. 2005, 110, E04016, doi:10.1029/2004JE002335.

Poulet, F., Bibring, J. P., Mustard, J. F., Gen-drin, A., Mangold, N., Langevin, Y., Arvid-son, R. E., Gondet, B., Gomez, C., and theOmega Team. Phyllosilicates on Mars andimplications for early Martian climate,Nature 2005, 438, 623–627, doi:10.1038/nature04274.

Quinn, R. C., Zent, A. P., Grunthaner, F. J.,Ehrenfreund, P., Taylor, C. L., Garry, J. R. C.Detection and characterization of oxidizingacids in the Atacama desert using the MarsOxidation Instrument, Planet. Space Sci.2005, 53, 1376–1388, doi:10.1016/j.pss.2005.07.004.

Rull P�rez, F., Martinez Frias, J. Raman spec-troscopy goes to Mars, Spectroscopy Europe2006, 18(1), 18–21.

Schulze-Makuch, D., Irwin, L. N., Lipps, J. H.,LeMone, D., Dohm, J.M., Fair�n, A. Sce-narios for the evolution of life on Mars,J. Geophys. Res. 2005, 110, E12S23,doi:10.1029/2005JE002430.

Sims, M. R., Cullen, D. C., Bannister, N. P.,Grant, W. D., Henry, O., Jones, R.,McKnight, D., Thompson, D. P., Wilson,

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P. K. The Specific Molecular Identificationof Life Experiment (SMILE), Planet. SpaceSci. 2005, 53, 781–791, doi:10.1016/j.pss.2005.03.006.

Skelley, A.M., Scherer, J. R., Aubrey, A. D.,Grover, W.H., Ivester, R. H.C., Ehren-freund, P., Grunthaner, F. J., Bada, J. L.,Mathies, R. A. Development and evaluationof a microdevice for amino acid biomarkerdetection and analysis on Mars, Proc. Natl.Acad. Sci. 2005, 102(4), 1041–1046,doi:10.1073/pnas.0406798102.

Squyres, S.W., Arvidson, R. E., Bell III, J. F.,Br�ckner, J., Cabrol, N. A., Calvin, W., Carr,M.H., Christensen, P. R., Clark, B. C.,Crumpler, L., Des Marais, D. J., d�ston, C.,Economou, T., Farmer, J., Farrand, W.,Folkner, W., Golombek, M., Gorevan, S.,Grant, J. A., Greeley, R., Grotzinger, J.,Haskin, L., Herkenhoff, K. E., Hviid, S.,Johnson, J., Klingelhçffer, G., Knoll, A. H.,Landis, G., Lemmon, M., Li, R., Madsen,M. B., Malin, M. C., McLennan, S.M.,McSween, H. Y., Ming, D.W., Moersch, J.,Morris, R. V., Parker, T., W. Rice, J.W., Jr.,Richter, L., Rieder, R., Sims, M., Smith, M.,Smith, P., Soderblom, L. A., Sullivan, R.,W�nke, H., Wdowiak, T., Wolff, M., Yen, A.The Opportunity Rover’s Athena scienceinvestigation at Meridiani Planum, Mars,Science 2004, 306, 1698–1703.

Squyres, S.W., Grotzinger, J. P., Arvidson,R. E., Bell III, J. F., Calvin, W., Christensen,P. R., Clark, B. C., Crisp, J. A., Farrand,W.H., Herkenhoff, K. E., Johnson, J. R.,Klingelhçffer, G., Knoll, A. H., McLennan,S.M., McSween, H. Y., Jr., Morris, R. V.,Rice, J.W., Jr., Rieder, R., Soderblom, L. A.In-situ evidence for an ancient aqueousenvironment at Meridiani Planum, Mars,Science 2004, 306, 1709–1714.

Tung, H.C., Bramall , N. E., Price, P. B. Mi-crobial origin of excess methane in glacialice and implications for life on Mars, PNAS2005, 102, 51, 18292–18296, doi:10.1073/pnas.0507601102.

Wang, A., Haskin, L. A., Squyres, S.W., Jolliff,B. L., Crumpler, L., Gellert, R., Schrçder, C.,Herkenhoff, K., Hurowitz, J., Tosca, N. J.,Farrand,W.H., Anderson, R., Knudson, A. T.

Sulfate deposition in subsurface regolith inGusev Crater, Mars, J. Geophys. Res. 2006,111, E02S17, doi:10.1029/2005JE002513.

Wang, A., Korotev, R. L., Jolliff, B. L., Haskin,L. A., Clumper, L., Farrand, W.H., Her-kenhoff, K. E., de Souza, P., Jr., Kusack,A. G., Hurowitz, J. A., Tosca, N. J. Evidenceof phyllosilicates in Wooly Patch, an alteredrock encountered at West Spur, ColumbiaHills, by the Spirit Rover in Gusev Crater,Mars, J. Geophys. Res. 2006, 111, E02S16,doi:10.1029/2005JE002516.

Wentworth, S. J., Gibson, E. K., Velbel, M. A.,McKay, D. S. Antarctic Dry Valleys and in-digenous weathering in Mars meteorites:Implications for water and life on Mars,Icarus 2004, 174, 383–395, doi:10.1016/j.icarus.2004.08.026.

Westall, F., Brack, A., Hofmann, B., Horneck,G., Kurat, G., Maxwell, J., Ori, G. G., Pillin-ger, C., Raulin, F., Thomas, N., Fitton, B.,Clancy, P., Prieur, D., Vassaux, D. An ESAStudy for the Search for Life onMars, Planet.Space Sci. 2000, 48, 181–202.

Williams, R.M.E., Malin, M. C. Evidence forlate stage fluvial activity in Kasei Valles,Mars, J. Geophys. Res. 2004, 109, E06001,doi:10.1029/2003JE002178.

Wynn-Williams, D. D., Edwards, H. G.M.Antarctic ecosystems as models for extra-terrestrial surface habitats, Planet. Space Sci.2000, 48, 1065–1075.

Wynn-Williams, D. D., Edwards, H. G.M.Proximal analysis of regolith habitats andprotective biomolecules in situ by LaserRaman Spectroscopy: Overview of terrestrialAntarctic habitats and Mars analogs, Icarus2000, 144, 486–503.

Wynn-Williams, D. D., Edwards, H. G.M.,Newton, E.M., Holder, J. M. Pigmentationas a survival strategy for ancient and modernphotosynthetic microbes under high ultra-violet stress on planetary surfaces, Internat.J. Astrobi. 2002, 1(1), 39–49.

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12.7Questions for Students

Question 12.1When searching for traces of past life on Mars, describe why it is important to

have access to “protected” environments – protected from what? Which sort of soilsshould a sampling device be able to obtain sample material from (hard, soft,porous, dust) and why?Question 12.2Assuming that the level of organics/organisms in the Martian soil is very small,

describe a strategy to maximize your chances for a positive detection. In a couple ofparagraphs, describe what you think is important.

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13Astrobiology Exploratory Missions and Planetary ProtectionRequirementsGerda Horneck, Andr� Debus, Peter Mani, and J. Andrew Spry

This chapter describes the legal and scientific issues of planetaryprotection requirements required for each space mission withinour Solar System. Planetary protection is based on an interna-tional treaty to prevent the introduction of microbes from theEarth to another celestial body or vice versa, whether this occursintentionally or unintentionally. Based on this treaty, a conceptof contamination control has been elaborated by the Committeeof Space Research (COSPAR) with regard to specific classes ofmission–target combinations, and it is recommended that eachspace-faring organization follow it. The intention of planetaryprotection is twofold: first, to protect the planet being explored andto prevent jeopardizing search-for-life studies, including those forprecursors and remnants, and second, to protect the Earth fromthe potential hazards posed by extraterrestrial matter carried on aspacecraft returning from another celestial body. Missions todifferent bodies in our Solar System that are of astrobiologicalinterest are considered with regard to planetary protectionrequirements.

13.1Rationale and History of Planetary Protection

Space activities started about 50 years ago, in 1957, when the first manmade objectreached outer space and broadcasted its signals around the world. With Sputnik –the name of this first satellite – a long-desired vision of mankind became reality,namely, the ability to leave the boundaries of our Earth and enter space. In parallelwith the rapid development of space activities that followed this first enterprise(1961, first cosmonaut in space; 1966, first safe robotic landing on the Moon withSurveyor 1; 1969, first human landing on the Moon), concern was raised aboutpossible contamination of the Moon and planets by terrestrial microorganisms.

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This concern was formulated by the National Academy of Sciences (NAS) of theUnited States as early as 1958:

“The NAS of the USA urges that scientists plan lunar andplanetary studies with great care and deep concern so that initialoperations do not compromise and make impossible forever aftercritical scientific experiments. For example, biological and radio-active contamination of extraterrestrial objects could easily occurunless initial space activities be carefully planned and conductedwith extreme care. The NAS will endeavor to plan lunar andplanetary experiments in which the Academy participates so as toprevent contamination of celestial bodies in a way that wouldimpair the unique and powerful scientific opportunities that mightbe realized in subsequent scientific exploration.”

Of course, such efforts to prevent contamination of the Moon and planets can beefficient only if they are followed globally by all space-faring nations.It took until 1967, with 10 years of meetings and consultations after the first

launch of a satellite, for the requirement for planetary protection to be incorporatedinto Article IX of the Outer Space Treaty of the United Nations (Treaty onPrinciples Governing the Activities of States in the Exploration and Use of OuterSpace, including the Moon and Other Celestial Bodies). The text reads as follows:

“States Parties to the Treaty shall pursue studies of outer space,including the Moon and other celestial bodies, and conduct ex-ploration of them so as to avoid their harmful contamination andalso adverse changes in the environment of the Earth resultingfrom the introduction of extraterrestrial matter, and wherenecessary, shall adopt appropriate measures for this purpose.”

This treaty has been signed and ratified by practically all space-faring nations. Itprovides that any of its parties can request consultation with any other partyconcerning the latter’s activities or experiments that might be harmful to the useof outer space. This treaty is the foundation on which all subsequent recommen-dations and guidelines of “planetary protection” (or “planetary quarantine,” a termused until 1975) are based.The rationale for planetary protection is the supposition that life could be a

universal or planetary phenomenon that emerges at a certain stage of either cosmicor planetary evolution, if the right environmental physical and chemical require-ments are present (see Chapter 1). Therefore, although the Earth is the only planetknown to harbor life, there may be many more habitable or even inhabited celestialbodies in our Solar System or beyond (see Chapter 6). With space exploration, wepossess for the first time the tools required to reach candidate moons and planetsin our Solar System by means of spacecraft and to search in situ for signatures ofindigenous life, either extinct or extant. However, the introduction – by means oforbiters, entry probes, or landing vehicles – and possible proliferation of terrestriallife forms on other planets could entirely destroy the opportunity to examine the

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target planets or moons in their pristine conditions. From this concern by thescientific community, the concept of planetary protection has evolved. Its intent istwofold:

• To protect the planet or moon being explored and to preserveits environment from terrestrial biological contamination inorder to prevent jeopardizing search-for-life studies, includ-ing those for precursors or remnants; this process is called“forward contamination prevention.”

• To protect the Earth and its biosphere and human populationfrom the potential hazards posed by extraterrestrial mattercarried on a spacecraft returning from another celestial body;this process is called “backward contamination prevention.”

In addition, planetary protection is concerned with the preservation of the proper-ties of the extraterrestrial samples themselves, as far as they are to be subjected toexobiological investigations, either in situ at the surface of the extraterrestrial bodyor when brought back to Earth. If correct and reliable preservation of the extra-terrestrial samples (or of parts of them) is not ensured, resulting in possiblecontamination by terrestrial organisms or a change in the properties of the samplematerial, one might draw false conclusions about the presence of extraterrestriallife forms or biohazards. The consequence of such mistreatment of extraterrestrialsamples could be either a false-positive result, requiring additional but unnecessaryplanetary protection measures, or a false-negative result, giving rise to free dis-tribution of potentially hazardous samples. False-negative results could endanger ahuman exploratory mission to a planet under consideration if the environment isinterpreted as harmless when in reality it is hazardous.

13.2Current Planetary Protection Guidelines

As previously noted, under the 1967 Outer Space Treaty of the United Nations, theexploration of the Solar System needs to be in compliance with a set of planetaryprotection constraints, for both outbound and inbound missions. These con-straints impose specific requirements on spacecraft design and construction,such as the introduction of sterilization procedures, integration under ultra-cleanor even sterile conditions, microbiological and cleanliness control, and the use ofhighly reliable systems in order to avoid crash landings. In the particular case ofsample return missions, the potential introduction of sample quarantine is alsoadded. Such requirements are required solely for planetary protection purposesand need to be considered right at the beginning of the planning of a mission to theplanets, moons, or small bodies (comets or asteroids) of our Solar System.The current planetary protection guidelines were developed by the scientific

community under the auspices of the Committee on Space Research (COSPAR)through its Panel on Planetary Protection. COSPAR was formed in 1958 by the

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International Council of Scientific Unions to coordinate worldwide space research.In this context, COSPAR also assumed responsibility for the contamination prob-lem. COSPAR is an observer at the United Nations Committee on Peaceful Uses ofOuter Space and reports to the United Nations through its periodic ScientificAssemblies.Concerning Planetary Protection, the current COSPAR policy is as follows:

“Although the existence of life elsewhere in the Solar System maybe unlikely, the conduct of scientific investigations of possibleextraterrestrial life forms, precursors, and remnants must not bejeopardized. In addition, the Earth must be protected from thepotential hazard posed by extraterrestrial matter carried by aspacecraft returning from another planet. Therefore, for certainspace mission/target planet combinations, controls on contami-nation shall be imposed, in accordance with issuances imple-menting this policy.”

This notation reflects that the current COSPAR policy is based on a scientificinterpretation of the Outer Space Treaty and that topics such as protection of theenvironment and ethical considerations are not covered. However, it is importantto note that all space-faring nations are bound to comply with the COSPAR policyand, consequently, with its recommendations. Hence, the planetary protectionguidelines of COSPAR shall be included in the relevant planetary protectiondocumentation of the various space agencies.The first planetary protection guidelines (developed by COSPAR in 1959 and

initially called COSPAR Objectives for Planetary Quarantine) were based onrelevant information about the probability of the survival and release of organismscontained either in or on exposed surfaces of spacecraft, about the surface andatmosphere characteristics of the planet under consideration, and about theprobable distribution and growth of the types of organisms involved. The firstrequirements for missions to Mars and other planets set by COSPAR, in 1964,imposed a maximum probability of 10–4 to find one viable microorganism perspacecraft (or one viable microorganism per 10 000 spacecrafts) and stated that theprobability of any unsterilized hardware crashing must be less than 3 · 10–5. Later,in 1969, the basic objective of the planetary quarantine was to achieve a probabilityof no more than 1 · 10–3 for contamination during the period of biological explo-ration. This period was assumed to be 20 years for Mars, starting from 1969 andextending through the end of 1988, and was assumed to include approximately100 missions. These numbers demonstrate the optimistic view that was taken atthe beginning of Solar System exploration. However, in this period, the onlysuccessful landings on Mars were the two Viking missions, and a further threelanders were sent to Venus (see Section 13.4).The early COSPAR concept of probability of contamination of a planet of

biological interest was replaced in 1989 by a concept of contamination control.This was to be elaborated specifically for certain space mission–target planetcombinations, such as orbiters, landers, or sample return missions. The current

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planetary protection recommendations, formulated by COSPAR through its Panelon Planetary Protection and in agreement with its own policy, separately considerthe target planet or body (including Solar System bodies encountered as flybysduring the mission) on one hand and the type of mission on the other:

• Concerning the extraterrestrial body to be explored, one has toconsider that, for instance, the risk of contaminating Mars isnot the same as that of contaminating Venus, because alanding mission to the latter planet, which has an ambientsurface temperature of more than 400�C, will already besufficiently sterilized during the landing process.

• Concerning the type of mission (orbiter, flyby, lander, orsample return), it is obvious that the contamination risk is notthe same for a spacecraft orbiting around a planet as for aprobe landing on its surface.

The current position is described in Table 13.1. This information is updatedperiodically by COSPAR in line with the best scientific advice.According to the scientific interest and mission goals for the different targets in

our Solar System, COSPAR’s planetary protection guidelines group missions intofive categories (see Table 13.1).

13.2.1Category I Missions

Category I missions include anymission (orbiters, flyby, or landers) to a target bodythat is not of direct interest for understanding the process of chemical evolution,origin of life, or other questions of astrobiology. The target bodies include theplanets Mercury and Venus, the Moon, and undifferentiated, metamorphosedasteroids and the Sun. However, other celestial bodies may be added to this listdepending on the scientific results obtained in the future. In category I, noprotection of the planets or bodies is warranted, and therefore no planetaryprotection requirements are imposed on the spacecraft and mission. Examplesinclude Smart I (targeting the moon) and Genesis (outbound – not encounteringany Solar System bodies).

13.2.2Category II Missions

Category II refers to all types of missions (orbiters, flyby, or landers) to targetbodies where there is significant interest relative to the process of chemicalevolution, but where there is only a remote chance that contamination carried bya spacecraft could jeopardize future exploration. Target planets and other bodiesinclude the giant planets Jupiter, Saturn, Uranus, and Neptune; the remote dwarfplanet Pluto with its moon Charon; comets; carbonous chondrite asteroids (theseasteroids contain a substantial amount of organic material); and the objects of the

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13 Astrobiology Exploratory Missions and Planetary Protection Requirements358

Table13

.1Current

COSP

ARplan

etaryprotection

catego

ries

withregard

tomission

sto

SolarS

ystem

bodies

andtype

sof

mission

s.

Category

CategoryI

CategoryII

CategoryIII

CategoryIV

CategoryV

Typeof

mission

Anybu

tEarth

return

Anybu

tEarth

return

Nodirect

contact

(flyby,som

eorbiters)Directcontact

(lan

der,prob

e,someorbiters)

Earth

return

Targetbo

dySee

text

[a]

See

text

[a]

See

text

[a]

See

text

[a]

See

text

[a]

Degreeof

concern

Non

eRecordof

plan

ned

impact

prob

ability

andcontamination

control

measures

Limiton

impact

prob

ability;p

assive

bioloadcontrol

Limiton

prob

ability

ofnon

-nom

i-nal

impact;lim

iton

bioload(active

control)

Ifrestricted

Earth

return:

Noim

pact

onEarth

orMoon;

returned

hardw

aresterile

;con

tain-

men

tof

anysample.

Ran

geof

requ

irem

ents

Non

eDocumen

tation

only:

PPplan

[b] ;pre-

launch

repo

rt;b

oost-

launch

repo

rt;p

ost-

encounterrepo

rt;

end-of-m

ission

repo

rt

Documen

tation

(cat-

egoryII

plus):con

-taminationcontrol;

organicsinventory;

implem

entingpro-

cedu

res(trajectory

biasing,

cleanroom

,bioloadredu

ction,

asnecessary)

Documen

tation

(categoryII

plus):

Pc[c]an

alysisplan

;microbial

redu

c-tion

plan

;microbial

assayplan

;or-

ganicsinventory;implem

enting

procedures(trajectorybiasing,

cleanroom

,bioload

redu

ction,

partialsterilization

ofcontacting

hardw

are,

bioshield,m

onitoring

ofbioloadviabioassay)

Outbou

nd:

Samecatego

ryas

target

body/outbou

ndmission

.Inbo

und:

Ifrestricted

Earth

return:

Documen

tation

(categoryII

plus):

Pcan

alysisplan

;microbial

redu

ction

plan

;microbial

assayplan

;trajectory

biasing;

sterile

orcontained

returned

hardw

are;

continual

mon

itoringof

projectactivities;p

roject

advanced

studies/research.

Ifunrestricted

Earth

return:N

one

aSe

eSection

13.4.

bPP:

Planetaryprotection

.cPc:

Probabilityof

contamination.

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Kuiper Belt. Again, other bodies may be added following new scientific results. Incategory II, the planetary protection recommendations require relatively simpledocumentation. The main requirement is to prepare a planetary protection planbefore the mission describing a brief pre- and post-launch analysis and whether itis planned to impact on the target – or whether this may happen accidentally. Inboth cases, a detailed description of impact strategies is required. Furthermore,reports are required after the encounter with the celestial body and at the end ofmission. These reports should give further details on the location of impact if suchan event occurred. Reporting of planned impact probability and contaminationcontrol measures is also required. Mission examples include Venus Express, Cassi-ni–Huygens (which had flybys at Venus, Earth, and Jupiter before arriving at theSaturnian system), and Stardust (which encountered the comet Wild 2).

13.2.3Category III Missions

Category III comprises certain types of missions (mostly flyby or orbiters) to atarget planet or body that – according to the current understanding – is of interestwith regard to chemical evolution and/or the origin of life or for which scientificopinion considers that a potential contamination with terrestrial microorganismscould jeopardize future biological experiments, e.g., those searching for signaturesof indigenous life. Our neighbor planet Mars and the Jovian moon Europa areclassified in this category. However, depending on future scientific results, otherbodies, especially other moons of the giant planets, may be included in thiscategory. It is important to note that an impact with the target body is not foreseenfor the missions of category III. However, if the probability of accidental impact issignificant, an inventory of the bulk constituent organics is required. In addition toa more extensive documentation than required in category II, for category III it isnecessary to assemble and test the spacecraft in a clean room, to monitor thebioburden (number of terrestrial microorganisms present) and reduce if necessary,and to include trajectory biasing. For instance, for orbital or flyby missions senttoward Mars, the spacecraft crash probability must be less than 1% during the20 years following the launch and 5% for the 50 years following the launch. For theJovian moon Europa, the crash probability must be less than 0.01%. Examplemissions include all the Mars orbiters (Mars Global Surveyor, Mars Odyssey, MarsExpress, Mars Reconnaissance Orbiter).

13.2.4Category IV Missions

Category IV missions are those missions of the utmost astrobiological interest.They include mostly entry probe or lander missions to a target planet of interestwith regard to chemical evolution and/or origin of life or for which scientificopinion provides a significant chance that contamination by terrestrial micro-organisms could jeopardize future biological experiments. As in category III, the

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celestial targets are Mars and Jupiter’s moon Europa, but in this case, missions tothe surface or subsurface are considered. For missions to Mars, depending on thelanding site and the scientific purpose of the mission, the following subcategoriesare defined.

• Category IVa: Mission with lander systems not carryinginstruments for the investigation of extant Martian life.

• Category IVb: Mission with lander systems carrying instru-ments for the investigation of extant Martian life.

• Category IVc: Landing mission to a special region, defined asa region within which terrestrial microorganisms are likely topropagate or a region that is interpreted to have a highpotential for extant Martian life forms. Given current under-standing, this category concerns regions where liquid water ispresent or may occur. Examples include subsurface access inan area and to a depth where the presence of liquid water isprobable, penetrations into the polar caps, or areas of poten-tial hydrothermal activity. At the time of writing (2006), un-certainty over what exactly constitutes a Martian “specialregion” is a subject of discussion within the Mars explorationcommunity. Clear guidance on this issue is required for theongoing mission set; some clarification can be expected fromwithin the community within the next few months and years.With regard to Jupiter’s moon Europa, the probability ofcontaminating Europa with one single viable microorganismmust be less than 0.01%.

For category IV missions, more detailed planetary protection documentation isrequired than for category III missions. The planetary protection requirementsinclude bioassays to enumerate the bioload, a probability of contamination analy-sis, an inventory of the bulk constituent organics, and an increased number ofimplementation procedures. The implementation procedures required includetrajectory biasing, clean-room assembly, bioburden reduction and monitoring,and, possibly, partial sterilization of the directly contacting hardware and a bio-shield for that hardware, depending on the subcategory considered. Pathfinder,Beagle 2, and the Mars Exploration Rover missions are all examples of category IVmissions.

13.2.5Category V Missions

Category V includes all missions within our Solar System that return to the Earth.The concern for these missions is the protection of the Earth and the Moon, whichare considered a single system (preventing back contamination). In this context,the Moon is to be protected from back contamination to retain freedom fromplanetary protection requirements on Earth–Moon travel.

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Return missions from all Solar System bodies are included in category V. Thoseclassified as “safe for Earth return” do not have constraints on handling or missiondesign. This is a risk-based decision, determined by scientific opinion when

• there was never liquid water in or on the target body,• metabolically useful energy sources were never present,• there was never sufficient organic matter (or CO2 or carbo-

nates and an appropriate source of reducing equivalents) in oron the target body to support life,

• the target body has been subjected to extreme temperatures(e.g., >160 �C),

• there is or was sufficient radiation for biological sterilizationof potential life forms, and

• there has been a natural influx to Earth (e.g., via meteorites) ofmaterial equivalent to a sample returned from the target body.

Missions from all other planets and moons of our Solar System are classified as“restricted for Earth return” and must follow the additional category V require-ments. The highest degree of concern is expressed by the absolute prohibition ofimpact upon return, the need for any returned hardware that directly contacted thetarget body to be sterile (contact chain breaking if sterilization is not possible), andthe need for containment of any non-sterilized sample collected and returned toEarth. In general, this concern is reflected in a range of requirements thatencompass those of category IV plus a continuing monitoring of project activities.Special research is required before the mission in order to develop suitable andefficient remote sterilization procedures and reliable containment techniques.The return elements of Genesis and Stardust are examples of “unrestricted-Earth-

return” category V missions. No restricted-Earth-return missions have flown sincethe development of the category-based planetary protection approach.

13.2.6Future Development of Planetary Protection Guidelines

It should be stressed that the COSPAR Planetary Protection Guidelines are a livingdocument that is steadily adapted to new findings on the habitability of the bodiesof our Solar System and new knowledge about terrestrial microbiology. Especiallyin view of the current and planned landing activities onMars (see Chapter 12), withrobotic and finally human visits, the planetary protection guidelines are currentlyunder review. For this purpose, the European Space Agency (ESA) and the Na-tional Aeronautics and Space Administration (NASA) have established PlanetaryProtection Advisory Groups gathering scientists from fields such as astrobiology,planetology, microbiology, hygiene, and sterilization technology. The priority taskof these groups is to advise the agencies concerning efficient planetary protectionmeasures for samples returned from Mars and for human exploratory missions,e.g., those landing on Mars. For human mission concepts, no planetary protectionguidelines have been developed by COSPAR to date.

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13.3Implementation of Planetary Protection Guidelines

Planetary protection considerations must be implemented very early in thedevelopment of a space mission to one of the bodies of our Solar System, becausethey may influence the design and integration of the final spacecraft and itsoperations. The initial starting point is the determination of the relevant categoryof the space mission–target planet combination (Table 13.1) and whether somesort of bioload control may be necessary. Usually the first formal recognition of arequirement is in the Planetary Protection Plan. Here, the planetary protectionrequirements and how the project plans to meet them are described. After thePlanetary Protection Plan is approved, generally by the planetary protection officerof the responsible space agency, a subsequent document, the Planetary ProtectionImplementation Plan, will give the detailed “how to” once the design is moreclearly understood.This approach can differ significantly from mission to mission, according to the

mission goals, complexity, and budgets (both funding and mass–volume budgets).However, planetary protection requirements need to be factored into the designprocess at an early stage (pre–phase A stage) of any mission to ensure compatibilitybetween the design and the COSPAR requirements. For smooth implementationof planetary protection overall, it is important to ensure that iterations of the designand planetary protection implementation proceed in an integrated fashion, suchthat changes in design are assessed for their impact on planetary protection andvice versa, ensuring that the planetary protection requirements are met by thespacecraft and instruments finally selected to fly. To train spacecraft engineers inplanetary protection issues, ESA and NASA regularly organize planetary protectioncourses for representatives of the space industry.As mentioned above, the first step is determining the category of the space

mission–target planet combination (Table 13.1). Of special concern with regard topreventing forward contamination are missions of categories III and IV. Depend-ing on the categorization, the following measures need to be implemented duringassembly until the final integration of a space system:

• The bioburden should be reduced by defined and validatedsterilization techniques.

• Assembly of biocleaned space systems should take place in aclean room with biological cleanliness control measures andbioload control.

• In order to avoid recontamination of the system after steri-lization, a cover to the space system as bioshield should beprovided; typically this will be jettisoned in flight.

• Terminal sterilization after final integration (through thebioshield using typically dry heat) should take place on a case-by-case basis, such as for category IVb or IVc missions toMars, e.g., the Viking mission.

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Most of the implementation procedures, as currently used, were originally devel-oped by NASA and are outlined in NASA documents. For example, the currentplanetary protection protocols for microbial examination, cleaning, and steriliza-tion of space hardware are largely based on Viking planetary protection state ofknowledge (i.e., from the 1970 s). Revision is currently underway because ourknowledge about microbial diversity and adaptive strategies has immensely in-creased since the Viking era (see Chapters 5 and 12) and because several interna-tional groups have now gained experience in microbial sampling from spacecraft(e.g., from Viking, Pathfinder,Mars Polar Lander, Beagle 2, Mars Exploration Rovers,Smart-1, Rosetta). In a series of workshops, international space agencies arecurrently revisiting these planetary protection protocols with the aim of amending

• the bioload measurements, by adding modern molecularbiology analysis methods, and

• the sterilization methods, by using modern methods such asthose from treatment of medical devices or pharmaceuticals.

13.3.1Bioload Measurements

Monitoring the bioload of a spacecraft is essential for determining the complianceof a project with the planetary protection guidelines issued by COSPAR. There areseveral reasons for knowing the number and type of microorganisms in andaround a spacecraft with regard to planetary protection issues:

• The data are the basis for determining appropriate steriliza-tion or cleaning procedures.

• The data will help us to understand the survival and growthpotential of microorganisms on the target planet or moon.

• If searching for signatures of life – especially extant life forms– is the goal of the mission, there is a need to know what typeof terrestrial microorganisms may be present on the space-craft.

• For sample returnmissions, it is required to know the bioloadof the outbound spacecraft in order to avoid false-positiveresults upon return to Earth.

The standardized, validated, culture-based microbial assay used by planetary pro-tection practitioners for determining the microbial bioload is given in the NASAdocument NPR 5340. For the sampling of microorganisms on the surface ofspacecraft, its subunits, or equipment within a spacecraft assembly facility, thestandard method includes either swabbing of multiple small areas (5 · 5 cm2) onand near the probe with sterile cotton swabs (Fig. 13.1) or wiping larger areas(1 m2) with a sterile wipe. The microorganisms are detached from the swabs/wipesby vortexing and sonication in distilled water or buffer, and part of the suspensionis spread on agar plates of a defined growth medium and aerobically incubated at32 �C or 37 �C. The colony-forming units (CFU) are counted every 24 h, and the

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overall bioload is estimated from the final count after 72 h of growth. Thisprocedure is based on a cultivation approach, allowing the detection of organismsable to grow under “standard” laboratory conditions.In order to determine the fraction of bacterial spores in the samples, a portion of

the suspension is heat shocked at 80 �C for 15 min before plating and incubation.This process, generally known as pasteurization, leads to inactivation of most of thevegetative bacterial cells, whereas bacterial spores and also cells of heat-tolerantmicroorganisms survive the heat treatment. It was found that spore formersconstitute the dominant fraction of microorganisms isolated from the surfacesof various spacecraft when the heat-shock method is used. These spore-formingmicrobes are of particular concern in the context of planetary protection, because inmany species their endospores can be highly resistant to a variety of environmentalextremes, including certain sterilization procedures and the harsh environment ofouter space or planetary surfaces (see Chapter 5). Among these environmentalisolates, strains have been identified that excel by an elevated resistance to variousphysical and chemical conditions, such as ionizing and UV radiation and desic-cation and oxidative stress, as compared to spores of related laboratory strains. It isspeculated that the laboratory strains may have lost their resistance because ofprolonged exposure to artificial laboratory conditions.In a study to further understand the spectrum of organisms present in spacecraft

environments, selected microbial species isolated from several spacecraft (MarsOdyssey, Smart, Rosetta lander) and their assembly facilities were identified using16S rDNA sequencing. This molecular biology method uses genomic DNA iso-lated from the cultures under investigation as template for amplification bypolymerase chain reaction (PCR). The phylogenetic relationship of the micro-organism is then determined by comparison of the individual 16S rDNA sequen-ces to other already-existing sequences in the public database. Among 45 Bacillusspore lines screened, 19 isolates showed high resistance to UV–C irradiation afterexposure to 1 000 J m–2 at UV–C of 254 nm. Using separate UV bands at the Mars-

13 Astrobiology Exploratory Missions and Planetary Protection Requirements364

Fig. 13.1 Swabbing of an area (5 · 5 cm2) ofa spacecraft subunit of the Mars ‘96 mission(photo credit: CNES).

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simulated solar constant including UV-A (315–400 nm), UV-(A+B) (280–400 nm),and full UV spectrum (200–400 nm), it was found that spores of Bacillus speciesisolated from spacecraft surfaces were more resistant to the Martian UV radiationclimate than a laboratory strain, B. subtilis 168. Such studies are important becausedust suspended in the Martian atmosphere can attenuate UV–C while allowingboth UV-A and UV-B to reach the surface. Among all Bacillus species tested, sporesof B. pumilus SAFR-032 showed highest resistance to all three spectral ranges ofsimulated Martian UV, compared to the other strains of the same species. In afurther study, representatives of these highly resistant spore formers will be testedunder the conditions of space and simulated Martian surface radiation for morethan one year in the EXPOSE facility of ESA, which will be attached to theInternational Space Station (see Chapter 11).Microorganisms in laboratory culture have very specific growth requirements,

e.g., with regard to temperature, oxygen availability, and pH value (see Chapter 5).Therefore, in order to determine themicrobial diversity of the bioload of a spacecraftor spacecraft assembly facility by laboratorymethods, the samples need to be dividedand subjected to a palette of different growth conditions with regard to pH, temper-ature, oxygen, and pasteurization (Fig. 13.2). In the ESA study “Determination of themicrobial diversity of spacecraft assembly facilities” the group of Rettberg obtainedthe following bioload results for the space missions Smart-1 and Rosetta. The vastmajority of colonies, about 96.7%, were identified after growth at a temperature of30�C. Only 3.2% grew at 5 �C and only about 0.1% (six in total) at 55�C. Seventy-twopercent of the colonies were formed under aerobic conditions and 28% underanaerobic conditions. Seventy-nine percent of the colonies were found on agar plateswith a pH of 7.0, 21% on agar plates with a pH of 9.0, and no colony at a pH of 4.5.The preference of one-fifth of the microorganisms for an alkaline environment(pH 9) could be the result of a selection due to detergents with a high pH that areused for routine cleaning of that particular clean room. In this study, about 66% ofthe colony-forming units originated from pasteurized aliquots of collected samples.Unlike sterilization, pasteurization is not intended to kill all microorganisms in thesample. Instead, pasteurization aims to achieve a reduction in the number of viableorganisms (e.g., in milk processing). The viability of thermotolerant or thermophilicmicroorganisms (for definition, see Chapter 5) as well as of especially robustdormant microbial forms such as bacterial spores is not impaired by pasteurization.Many isolates from pasteurized samples could be identified as eitherBacillus speciesor asMicrococcus species. BecauseMicrococcus does not form spores, it is not strictlycorrect to describe all survivors of the pasteurization process as spores (as iscurrently assumed in the planetary protection guidelines).In summary, it can be noted that a large fraction of the microorganisms

(58–75%) isolated from spacecraft or space assembly facilities is considered tobe indigenous to humans and was brought into the facility by the workers assem-bling the spacecraft. The majority of these isolates belong to the Staphylococcus orMicrococcus groups. This fraction of the overall bioload could be reduced byappropriate training of the personnel and controlling of the working procedures.The remaining fraction (25–42%) of the bioload either is associated with soil and

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dust (Bacillus group) or originates from the specific environment and is deter-mined mainly by the clean-room class of the spacecraft assembly facility.

13 Astrobiology Exploratory Missions and Planetary Protection Requirements366

Fig. 13.2 Plating scheme with a broad range of cultivationconditions for the detection of microorganisms, isolated fromspacecraft or spacecraft assembly facility within the ESA projectMiDiv (Rettberg et al. 2006).

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So far, most work on bioload control has been restricted to cultivable micro-organisms. However, it is well known that many microorganisms found in envi-ronmental samples are not readily cultivable in the laboratory. Use of new tech-nologies, e.g., fluorescent DNA staining of bacterial cells or epifluorescence micro-scopy, has shown that the number of microorganisms in aquatic environments is100–1000 times greater than that determined by cultivation techniques. These so-called non-cultivable microorganisms (we probably have not yet found the correctcultivation conditions) are assumed to represent the majority of terrestrial micro-organisms.Although these organisms cannot be cultured today, they can still be detected

and described by analyzing their biomolecules. One way to bypass the cultivationlimitation is to focus on the detection of specific DNA sequences as markermolecules for microorganisms present. PCR is a powerful molecular tool to detecteven minute amounts of specific unknown DNA sequences. This technique isnow being applied to detect and identify very low numbers of microorganismspresent in environmental samples, such as those from spacecraft or their assem-bly facilities. In addition, when the right target gene is chosen for analysis, thistechnique may be used for classifying the taxa or even species of the non-cultivable organisms. Highly conserved genes such as those of the 16S rRNAare suitable targets for phylogenetic identification of prokaryotes. A major advant-age of this approach is that a large databank of sequenced 16S rDNA is alreadyavailable.Other techniques to track non-cultivable microorganisms include Live/Dead

fluorescence analysis, the ATP bioluminescence assay as an indicator of live cells,or assays for lipopolysaccharides (e.g., the limulus amebocyte lysate [LAL] assay)as membrane building blocks for detecting microorganisms of the Bacteriadomain. However, each of these assays has limitations that mediate against beingused as a direct replacement for the classical spore assay. For example, the LALmethod does not detect gram-positive bacteria or representatives of the Archaeadomain, because of the specific membrane components detected by the assay (seeChapter 5).

13.3.2Bioburden Reduction

It is normal aerospace practice for spacecraft to be assembled in clean rooms.These rooms have specific air filtration installations to keep the concentration ofparticles low. They are used for processing space hardware requiring a high degreeof cleanliness. Planetary protection requirements go over and above these space-craft-specific requirements and are dictated by the category of the mission.Research in the Viking era showed that, depending on the class of the clean

room, a lower limit of background surface bioload density can be assumed (Table13.2). Below this level, further reductions are not possible because of the erratic andnon-uniform nature of microbial contamination and the ever-present risk of cross-contamination by the activities of clean-room operators and operations.

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Table 13.2 Lower limit of surface bioload density in clean roomsof different classes.

Room classification Surface bioload density

Uncontrolled manufacturing 1 · 105 spores m–2

Class 100 000 clean room with normal controls 1 · 104 spores m–2

Class 100 000 clean room with stringent controls 1 · 103 spores m–2

Class 10 000 clean room with normal controls 5 · 102 spores m–2

Class 10 000 clean room with stringent controls 5 · 101 spores m–2

Category I and category II missions generally do not need special measures ofbioload reduction. Category III missions are orbital or flyby missions sent to targetsof high astrobiological interest, such as Mars or Jupiter’s moon Europa, andrequire bioburden reduction if the mission cannot meet the trajectory biasingrequirements (i.e., crash probability of <1% for 20 years after launch and <5% for50 years after launch). In this case, the total bioload of the spacecraft must bereduced to a level lower than 500 000 bacterial spores. This requirement includesexposed external and internal surfaces as well as mated and encapsulated biobur-den.Category IV missions are surface-landing missions to Mars or Jupiter’s moon

Europa that require sterilization or biocleaning of lander-exposed surfaces (sum-marized in Table 13.3) in order to comply with the following levels:

• For systems landing on the surface of Mars but not carryinginstruments for the investigations of putative extant Martianlife forms, the level of contamination shall be less than300 bacterial spores m–2 and less than 300 000 bacterialspores per lander concerning exposed external and internalsurfaces. These numbers are based on the contaminationlevel determined for the Viking lander before sterilization(Viking pre-sterilization level) and apply to category IVamissions.

• For systems landing on the surface of Mars and carryinginstruments for the investigation of extant Martian life, thecontamination level shall be reduced by four orders of mag-nitude, compared to landing systems without life-detectionexperiments. The resulting “calculated” number is less than30 bacterial spores per lander, which corresponds to theViking lander post-sterilization levels. In cases where thenature and sensitivity of a particular life-detection experimentrequires a more stringent bioburden reduction, then theseshall be the driving requirements. These levels of bioburdenreduction apply to category IVb missions.

• Landing missions to a “special region” of Mars, even if theydo not include life-detection experiments, shall also comply

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with Viking lander post-sterilization biological levels, accord-ing to the category IVc mission requirements. If the landingsite is within the special region, the entire landed system shallbe sterilized at least to Viking post-sterilization biologicalburden levels. If the special region is accessed though hori-zontal or vertical mobility, this high level of sterility appliesnot necessarily to the whole lander but to those parts orsubsystems that will be in contact with the special region.If an off-nominal condition (such as a hard landing) wouldcause a high probability of inadvertent biological contami-nation of the special region by the spacecraft, the entirelanded system must be sterilized to Viking post-sterilizationbiological burden levels.

• For any missions sent toward Jupiter’s moon Europa,the probability of contaminating this body with terrestrialmicroorganisms shall be less than 10–4.

Table 13.3 Current bioburden reduction requirements for Marslanders (Viking pre- and post-sterilization levels for surface andembedded bioburden)

Requirement Category of mission

IVa: Viking IVa: Viking IVb: VikingPre-sterilization Pre-sterilization with

impacting hardwarePost-sterilization

Surface spore density 300 spores m–2 300 spores m–2 No explicitrequirement

Total surface spores 3 � 105 3 � 105 30[a]

Total spores (including surface,mated and embedded)[c]

[b] 5 � 105 [b]

Source: U. S. Space Studies Board Report, “Preventing the Forward Contamination of Mars.”a No surface spore assays required; number of spores established by the application of a

certified bioburden reduction method (dry heat).b No numerical requirements on embedded burden except for spacecraft with impacting

hardware (e.g., heat shields). Embedded bioburden is assumed to remain embedded undernominal operations.

c Embedded bioburden refers to bioburden buried inside non-metallic spacecraft material.

All spacecraft integration operations must be performed in an ISO class 8 cleanroom (ISO 14644–1: Clean Rooms and Associated Controlled Environments, Part1: Classification of Air Cleanliness) or better, with biological contamination mon-itoring. Periodic microbiological assessments must be performed on the flighthardware in order to check the contamination level. If the contamination is toohigh, surface biocleaning must be performed during integration. The traceability

13.3 Implementation of Planetary Protection Guidelines 369

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of all monitoring must be kept and the final assessments must demonstrate thatthe specification is met. After the last integration step, measures are taken in orderto prevent any recontamination. As for orbiters, any unfortunate crash impactmust be located, and organic materials brought to Mars must be known andrecorded.In order to comply with the contamination levels required for a certain category,

the following cleaning or sterilization measures are applied during and after theassembly of the equipment and/or at the final integration:

• surface wiping with biocleaning agents,• gamma radiation sterilization,• dry-heat sterilization, and• hydrogen peroxide gas plasma sterilization.

The selection of the appropriate cleaning and sterilization method (Table 13.4) isdriven by two requirements: Firstly, the chosen method and associated proceduresmust be able to reach the specified decontamination level, and secondly, theyshould not affect the functional performance of the treated equipment.

Table 13.4 Bioburden reduction and sterilization methods usedfor the Mars ‘96 lander.

Bioburden reduction orsterilization method

Spacecraft subsystem of concern

Biocleaning[a] Finnish, U. S., Russian experiments on small stations;some subsystems and housekeeping systems of smallsurface stations and penetrators

Gamma-ray sterilization Landers parachute and airbags systems; some sub-systems of small stations and penetrators

Dry-heat sterilization Finnish meteorological sensor of the small stationsH2O2 gas plasma sterilization French payload on small stations; penetrators; some

subsystems of the penetrators

a Alcohol, sporicide, UV, class 100 clean room.

However, below a certain level of cleanliness (<300 spores m–2), the direct culturingand counting methodology is not sensitive enough for enumerating spacecraftbioburden. For this reason, a series of parametric measures were developed byNASA during the 1960 s. These can be used to estimate the bioload of spacecraftsterilized by dry heat (given as appendices in NASA document NPR8020.12C)based on parametric measurements and estimates. These include

• Time-temperature for sterility: A surface with a temperatureexceeding 500�C for more than 0.5 s during the mission maybe considered sterile (viable microbial bioload statisticallyzero).

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• D value, Z value: Dry-heat microbial reduction at a relativehumidity less than 25% (referenced to 0 �C and 1 000 hPa) forspores has a D value (the time for a 10-fold reduction ofsurvival at a certain temperature) at 125 �C of 0.5 h for freesurfaces and of 1 h for mated surfaces. The correspondingZ value (the change in temperature for a change in the Dvalue by a factor of 10) is 21 �C for the temperature interval104–125�C.

• Hardy organisms: The maximum reduction factor that maybe taken for a dry-heat microbial reduction is 104. This pa-rameter specification is based on an assumed fraction ofhardy organisms (these are of higher resistance to the processthan the general microbial population) of 10–3 and a reductionof only 0.1 in a nominal sterilization cycle.

• Surface microbial density: Various parameter specificationswere permitted for microbial bioload estimates where assaysare not feasible; these may also eliminate the need for assay(Table 13.2).

13.3.2.1 Surface Wiping with Biocleaning AgentsCleaning by wiping techniques in the spacecraft assembly facility shall be per-formed as often as necessary, depending on the bioburden assessed on surfaces(however, at least every day). A typical cleaning agent is isopropyl alcohol (IPA).This agent is not sporicidal, i.e., it does not kill spores; however, it adequatelycomplies with the bioburden reduction specifications and is used to remove – butnot kill – spores from the wiped surfaces. Sporicides may be used in order to kill theremaining microorganisms that are not removed from surfaces by the wipingtechnique; however, these may leave a residue, and such procedures need to beperformed in conjunction with the contamination control staff for the spacecraft.Microbiological assessments must be continued according to a standard protocol inorder to verify that the surface biocontamination level remains within acceptablelimits.

13.3.2.2 Gamma Radiation SterilizationGamma radiation sterilization results from the interaction of photons in the rangeof 1.17–1.33 MeV (issued from high-activity radioactive 60Co sources) with livingsystems. Such photons are able to penetrate several centimeters into steel. Thetypical dose is 25 kGy, which is sufficient to kill spores of the reference micro-organism Bacillus pumilus, known as the most radiation-resistant representative ofbacterial spores. Sterilization with gamma irradiation requires a few minutes to afew hours, depending on the activity of the source and the radiation dose required.Gamma sterilization must be conducted in a special certified blockhouse in orderto protect the operators and the environment. Because of its limited compatibility

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with space hardware – in particular with electronics, optics, and some organicmaterials – this technique is suitable mainly for structural elements or for radia-tion-compatible subsystems, which may include, for example, airbags and/orparachutes.

13.3.2.3 Dry-heat SterilizationDry-heat thermal sterilization has been the technology most often used for space-craft sterilization since the 1970 s, when it was applied as a terminal sterilizationprocess on the Viking landers after their final integration. The fully integratedViking landers encased in the bioshield were sterilized at 112 – 1.7 �C for 30 h. Thisfinal dry-heat sterilization was applied after the lander was biocleaned to a level of300 bacterial spores m–2 and after the life-detection instruments were sterilized at120 �C for 54 h. Dry-heat cleaning is presently the only method qualified for spacehardware sterilization by NASA. The optimal range recommended is 104 �C to125�C for 50 h and 5 h, respectively. The effects of thermal sterilization on micro-organisms depend on the profile of temperature and time during the sterilizationprocess. The typical parameters used for medical sterilization are given for sporesof the reference microorganisms Bacillus subtilis or Bacillus stearothermophilus. Themedical procedures generally give temperatures between 105�C and 180�C, forperiods between 1.5 and 300 h. However, not all spacecraft material and equipmentcan withstand dry-heat sterilization; for example, modern spacecraft batterieswould be destroyed by heat treatment at well below the minimum sterilizationtemperature.

13.3.2.4 Hydrogen Peroxide Vapor/Gas Plasma SterilizationHydrogen peroxide gas plasma is a recent sterilization method developed byindustry for sterilization of medical instruments. The so-called Sterrad sterilizationprocess is done in specific sterilization chambers at low temperature (45 �C) andlow pressure (less than 1 hPa) where gaseous hydrogen peroxide sterilizes theequipment surface during a relatively short period (less than 1 h). Final plasmamay be generated in order to increase the effect of sterilization and to break theremaining hydrogen peroxide molecules. The U. S. Food and Drug Administrationsuccessfully tested the effect of 50 sterilization cycles on different medical devices,including electronic and optical instruments. The medical procedures are qualifiedfor spores of the reference microorganism Bacillus subtilis var. niger. Concerningspacecraft sterilization, this method was first tested (without the plasma phase) in1992 on different materials and equipment of theMars ‘96mission (Table 13.4). Itwas found to be very compatible with various kinds of equipment. Later, elementsof the Beagle 2 spacecraft were sterilized using this technology. However, uncer-tainties about the compatibility of the process with complete spacecraft, togetherwith the fact that this is a surface-only sterilization technology, have slowed itswidespread adoption in the spacecraft community.

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13.3.3Prevention of Recontamination

One of the main problems during the spacecraft integration process is maintainingbiological cleanliness after sterilization of the equipment. A special protocol isrequired to ensure that the spacecraft assembly facility is maintained in a bio-logically clean condition. This protocol must, on one hand, comply with requiredoperations and access procedures for equipment and workers and, on the otherhand, prevent recontamination of the sterilized equipment. To achieve this goal,various approaches can be adopted. Controlled access to the sterile clean room withoperators being required to wear decontaminated overshoes, overalls, hoods,masks, and gloves is typical. Sterile tools need to be used, and continuous mon-itoring of the bioload level and frequent biocleaning operations must be includedin the protocol. One example of this approach is the planetary protection protocolused for theMars ‘96mission. In this case, two ISO class 5 clean rooms were used.To control and maintain the cleanliness of the clean rooms, all working surfaces(tables, chairs, etc.) in the integration area were cleaned daily with alcohol and a

13.3 Implementation of Planetary Protection Guidelines 373

Fig. 13.3 Integration of Mars lander space-craft. (a) Mars ‘96 lander in a biologicallycontrolled environment in NPO LavochkinMoscow (Photo credit: CNES). (b) MarsPathfinder at the Spacecraft Assembly Facility

of the Jet Propulsion Laboratory (Photo cour-tesy of R. Koukol, JPL). (c) Beagle 2 in the class10 clean room of the Open University, U. K.(photo courtesy of Open University).

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sporicide, and operators had to wear clean-room garments (Fig. 13.3). The clotheswere washed in chlorinated water solutions, and one wash in 10 was followed bysteam sterilization (20 min at 120 �C).However, the prevention of contamination does not end with spacecraft assem-

bly. Little or no recontamination should occur during launch. This can be achievedby encasing the spacecraft in a biobarrier or bioshield and removing this shieldonly after the system is launched into space.

13.4Astrobiology Exploratory Missions of Concern to Planetary Protection

Within the ongoing and planned ventures to explore the planets, moons, andother bodies of our Solar System, both by orbiters and robotic landing missions,the search for signatures of life beyond the Earth is one of the major drivers. Inthe selection of candidate targets for this enterprise, the overarching argument isthe putative habitability of the planet or moon under consideration (see Chap-ter 6). The planetary protection requirements are based on these considerations(Table 13.1).

13.4.1Missions to the Moon

In preparation for the first landing mission to the Moon within the Apollo program,planetary protection regulations with regard to the possible contamination of acelestial body, in this case the Moon, were considered for the first time. However,because of the surface conditions, such as high vacuum and intense cosmic andsolar UV radiation, the Moon’s surface was regarded as highly unfavorable for thegrowth of terrestrial microorganisms. In contrast, the absence of oxygen, water,and other life-supporting substances was thought not to prohibit survival, espe-cially of dormant anaerobic microorganisms. It was considered that the ubiquitousnature of bacterial spores and their durability under adverse conditions, includinghigh vacuum and low temperatures (see Chapter 5), must be fully appreciated toprevent contamination. It was argued that a biological contamination of the Moonmight affect studies on the early history of the Solar System, the origin of life onEarth, extraterrestrial life, and the chemical composition of matter in the remotepast. Especially in order to avoid possible distortion of chemical evidence bymicrobial action and contamination of the Moon’s deeper layers, it was recom-mended

• to minimize contamination to the extent technically feasible;• to inventory all organic chemical constituents brought to the

surface of the Moon; and• to perform sterile drilling on the Moon in order to return an

uncontaminated sample of the lunar subsoil for biologicaland geochemical investigations.

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The latter recommendation shows that, at that time, it was not excluded that lifemight exist at some depth below the surface of the Moon where temperatures neverexceed 100�C and UV radiation does not penetrate.Because minute traces of Earth-borne contaminants could lead to completely

erroneous interpretations, the samples of rock and soil brought back from theMoon needed to be carefully protected. For this purpose, the Lunar ReceivingLaboratory was set up at the Manned Spaceflight Center (now Johnson SpaceflightCenter) in Houston, USA, where lunar samples were cataloged and subjected topreliminary examination. The in vitro and in vivo tests at the Lunar ReceivingLaboratory provided data showing that no microorganisms were recovered fromthe lunar samples returned during the Apollo program. This was a result of boththe efforts to limit contamination in the earlier unmanned launches and the effortsto take the samples under aseptic conditions in the Apollo manned landings. Thecontamination control plan developed and implemented eventually resulted inproviding investigators with lunar samples containing less than 0.1 ppm totalterrestrial organic contamination. It should be noted that this is as low as oreven lower than the experimental blanks obtained in organic geochemistry re-search laboratories.Another concern of back-contamination arose from the astronauts themselves

who had landed on the lunar surface. Flight plans called for the astronauts tocontain as much lunar dust as possible in the lunar module (LM) by vacuuming itoff their space suits then removing the suits and sealing them in storage bagsbefore returning to the command module (CM). During the transfer from theMoon to Earth, the LM pressure relief valve was opened and the oxygen flow in theCM was increased to maintain a current of gas flowing from the CM to the LM,thus minimizing the amount of dust carried into the CM. After return to the Earth,the crew of the first two Apollo landing missions was isolated in a Mobile Quar-antine Facility aboard the recovery ship (Fig. 13.4), before being held in quarantine

13.4 Astrobiology Exploratory Missions of Concern to Planetary Protection 375

Fig. 13.4 Apollo 11 astronauts (from left toright) Neil A. Armstrong, commander; MichaelCollins, command module pilot; and Edward E.Aldrin, Jr., lunar module pilot, as they areconfined to the Mobile Quarantine Facilityaboard the U. S. S. Hornet, prime recovery shipfor the historic Apollo 11 lunar landing mission(Photo NASA).

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in the living quarters at the Lunar Receiving Laboratory for at least three weeks. Inlight of the results from the first two Apollo missions, the requirements for crewquarantine of Apollo astronauts were discontinued for the follow-on lunar mis-sions. However, the biological containment practices in the Lunar ReceivingLaboratory and the biological examination of the lunar samples were continuedbecause, among other things, they assured the integrity of the samples.There are reports that bacteria might have survived for 2.7 years on the surface of

the Moon in the polyurethane foam insulation of the camera interior of theSurveyor 3 spacecraft. This lander was visited by the crew of the Apollo 12 LM,and about 10 kg of parts from the Surveyor 3 spacecraft, including the TV camera,were removed for later examination back on Earth. Whereas most samples turnedout to be sterile, the bacterium Streptococcus mitis was isolated from one part of thecamera foam. Although it was first concluded that the bacterium was of terrestrialorigin and had survived the lunar exposure and return trip, there are manyindications that it came from contamination of the sample during the collectionor return trip. The main reason is that S. mitis was identified as part of themicroflora of the astronauts of Apollo 12.The present view is that the Moon is part of a single Earth–Moon system; hence,

from a planetary protection perspective the Moon does not need to be protectedfrom terrestrial biological contamination. However, the Moon must be protectedfrom contamination by extraterrestrial samples, defined as “restricted Earth re-turn” of category V missions, in order to retain freedom from planetary protectionrequirements on future human lunar missions, including the establishment of alunar base.

13.4.2Missions to Mars

With the exception of the Earth, Mars is by far the most intensively studied of theplanets of our Solar System (Table 13.5). In 1972, for the first time a spacecraft,Mariner 9, passed over the younger parts of Mars, revealing a wide variety ofgeological processes as indicated by volcanoes, canyons, and channels that resem-ble dry river beds and attest to a stable flow of water on Mars at some time in thepast and even in more recent times (see Chapter 8). The COSPAR PlanetaryProtection Guidelines categorize missions to Mars within category III, IV, or V,depending on the kind of mission (whether they are orbiters, flyby missions,landers with in situ research, or landers with sample return tasks) (Table 13.1).

13.4.2.1 Orbiters or Flyby Missions to MarsCurrently four spacecraft are orbiting Mars: Mars Global Surveyor, Mars Odyssey,and Mars Reconnaissance Orbiter of NASA, and Mars Express of ESA (Table 13.5).They are categorized as category III missions. If they achieve a total bioburden ofless than 500 000 spores per total spacecraft, then they do not need trajectorybiasing.

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Table 13.5 List of past and present missions to Mars.

Mission Country/Agency

Launchdate m/d/y

Purpose Results

Marsnik 1 USSR 10/10/60 Mars flyby Did not reach Earth orbitMarsnik 2 USSR 10/14/60 Mars flyby Did not reach Earth orbitSputnik 22 USSR 10/24/62 Mars flyby Achieved Earth orbit onlyMars 1 USSR 11/1/62 Mars flyby Radio failed at 106

million kmSputnik 24 USSR 11/4/62 Lander Achieved Earth orbit onlyMariner 3 U.S. 11/5/64 Mars flyby Shroud failed to jettisonMariner 4 U.S. 11/28/64 First successful Mars flyby 7/14/65 Returned 21 photosZond 2 USSR 11/30/64 Mars flyby Passed Mars but radio

failed; returned no plane-tary data

Mariner 6 U.S. 2/24/69 Mars flyby 7/31/69 Returned 75 photosMariner 7 U.S. 3/27/69 Mars flyby 8/5/69 Returned 126 photosMariner 8 U.S. 5/8/71 Mars orbiter Failed during launchCosmos 419 USSR 5/10/71 Mars lander Achieved Earth orbit onlyMars 2 USSR 5/19/71 Mars orbiter/lander arrived

11/27/71No useful data, landerdestroyed

Mars 3 USSR 5/28/71 Mars orbiter/lander, arrived12/3/71

Some data and a few photos

Mariner 9 U.S. 5/30/71 Mars orbiter, in orbit11/13/71 to 10/27/72

Returned 7 329 photos

Mars 4 USSR 7/21/73 Mars orbiter Flew past Mars 2/10/74Mars 5 USSR 7/25/73 Mars orbiter, arrived 2/12/74 Lasted a few daysMars 6 USSR 8/5/73 Mars orbiter/lander, arrived

3/12/74Little data returned

Mars 7 USSR 8/9/73 Mars fly by /lander, arrived 3/9/74 Little data returnedViking 1 U.S. 8/20/75 Mars orbiter/lander, orbit 6/19/76–

1980, lander 7/20/76–1982Combined, the Viking or-biters and landers returnedmore than 50 000 photos

Viking 2 U.S. 9/9/75 Mars orbiter/lander, orbit8/7/76–1987, lander 9/3/76–1980

Combined, the Viking or-biters and landers returned>50 000 photos

Phobos 1 USSR 7/7/88 Mars/Phobos orbiter/lander Lost 8/88 en route to MarsPhobos 2 USSR 7/12/88 Mars/Phobos orbiter/lander Lost 3/89 near PhobosMars Observer U.S. 9/25/92 Orbiter Lost just before Mars arrival

8/21/93Mars GlobalSurveyor

U.S. 11/7/96 Orbiter, arrived 9/12/97 Science mapping

Mars ‘96 Russia 11/16/96 Orbiter and landers Launch vehicle failedMars Pathfinder U.S. 12/4/96 Mars lander and rover, landed

7/4/97Last transmission 9/27/97

Nozomi (Planet-B) Japan 7/4/98 Mars orbiter, currently in orbitaround the Sun

Mars fly-by due to propul-sion problem

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Mission Country/Agency

Launchdate m/d/y

Purpose Results

Mars ClimateOrbiter

U.S. 12/11/98 Orbiter Lost on arrival at Mars9/23/99

Mars Polar Lander/Deep Space 2

U.S. 1/3/99 Lander/descent probes toexplore Martian south pole

Lost on arrival 12/3/99

Mars Odyssey U.S. 4/7/01 Orbiter Science mappingMars Express withBeagle 2

ESA 6/2/03 Orbiter and lander Science mapping by orbiter,lander lost on arrival

Mars ExplorationRovers MER Aand B

U.S. June/July2003

Lander and rover Landed on 1/4/04 (MER A);on 1/25/04 (MER B);extended science mission

Mars Reconnais-sance Orbiter

U.S. 8/12/05 Orbiter Entered orbit around Mars3/10/06

For the historic mission set, Mars Global Surveyor, Mars Odyssey, and Mars Expressadopted the trajectory biasing approach. Mars Reconnaisance Orbiter was requiredto adopt the bioburden control approach, as the mission design required a lowscience orbit that was too “risky” to meet the probability of impact requirements forthe first 20 years of the mission.

13.4.2.2 Landers or Rovers with in Situ MeasurementsAll lander missions to Mars fall into category IV. Table 13.5 shows that there wereat least five successful landing events on Mars, namely, Viking 1 and Viking 2,MarsPathfinder, and the two Mars Exploration Rovers Spirit and Opportunity. However,those lander missions that failed needed to follow the same stringent planetaryprotection requirements (Table 13.1).The Viking landers themselves, with their overarching goal of searching for

signatures in indigenous microbial life on the surface of Mars, were terminallysterilized. That is, at the end of the assembly phase, the landers were subjected to ahigh-temperature dry-heat sterilization process of 112 – 1.7 �C for 30 h, renderingthem effectively sterile (with a bioburden close to 0; statistically, 30 spore-formingmicroorganisms were accounted at launch).However, when the scientific findings of the Viking landers showed that the

Martian environment is inhospitable to then-known terrestrial microorganisms,COSPAR requirements for Martian landers carrying non-life-detection instrumen-tation (now category IVa) were relaxed to the level of contamination present on theViking landers before sterilization, namely, 300 000 spore-formingmicroorganismsin total, at an average density of below 300 microorganisms per square meter for asingle landing event. To achieve even this level of cleanliness is not straightforwardand requires spacecraft assembly in a clean-room environment, with a set ofmonitoring and cleanliness criteria over and well above those normally adoptedfor spacecraft assembly, e.g., with missions into low Earth orbit. However, for

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landers carrying extant life-detection instrumentation (category IVb), the “goldstandard” continues to be that of the contamination present on the Viking landerspost-sterilization, namely 30 spores or fewer (Table 13.3).Therefore, sinceViking, all NASA (Pathfinder,Mars Polar Lander, Mars Exploration

Rovers Spirit andOpportunity) and ESA (Mars ‘96,Beagle 2) missions to the surface ofMars (Table 13.5) have been classified as category IVa missions. (The SovietMars 3lander successfully landed onMars in December 1971, but contact was lost 20 s afterthe landing.) NASA’s 2007 Phoenix mission was categorized as IVa, but it meetscategory IVc requirements for its targeted landing site, which is a polar region rich inwater ice. NASA’s 2009Mars Science Laboratory is assigned category IVc. ESA’s 2013ExoMars mission (see Chapter 12) has yet to be formally categorized.For some missions, the scientific studies could potentially be affected or com-

promised by contaminants carried by the spacecraft. In these cases, the scienceteam negotiates with the mission management to request additional requirementsin terms of, e.g., chemical cleanliness over and above those of planetary protection.These are typically detailed in the Planetary Protection Implementation Plan. Theycan involve materials control in the lander and spacecraft assembly facility, togeth-er with monitoring of the organic compounds that would normally be “permitted”in the spacecraft. These scientific cleanliness requirements impact the environ-mental control of the spacecraft from initial assembly through launch. The Beagle 2spacecraft (Table 13.5) was one such mission. For the upcoming Mars ScienceLaboratory (MSL09) mission, an organic cleanliness level, measured as total or-ganic carbon (TOC), of less than 1 ng cm–2 is required for all equipment that willcome in contact with Mars samples.As an example, the Beagle 2 lander mission will be used to demonstrate how

problem areas were identified during the design and construction of the lander andhow final solutions were found (Table 13.6).Once the scope of the planetary protection problem is understood, a sterilization

strategy can be developed for a specific mission. This could rely on a singletechnology or on several and may require a single processing of the hardware orseveral. In the case of Viking, multiple dry-heat processings were used. For the MarsExploration Rovers, typically only one dry-heat processing was used. In contrast, theBeagle 2 program used several sterilization technologies, developing a “preferencecascade” where gamma irradiation is preferred after dry heat, as it is also apenetrating technology. Hydrogen peroxide–based methodologies were next inpreference because of their benign effect on the hardware. However, this technologysterilizes only surfaces. Finally, IPA (or other solvent) wiping is the last approach, asit removes the organism rather than killing it in situ and is used only as a last resort.Ideally, combinations could be used, although it is quite challenging to determinewhether all the components of one system are compatible with a single technology.The combination of parametric measures and culture-derived estimates of

bioload is then summed to give the final bioburden at launch, and this is checkedversus the requirement before launch is permitted. Table 13.7 gives the finalbioload numbers from three Mars lander missions where very different planetaryprotection strategies were employed.

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13 Astrobiology Exploratory Missions and Planetary Protection Requirements380

Table13

.6Beagle2sterilization

challeng

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high

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inthePlan

etaryProtection

Plan

.

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give

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Steriliz

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ence

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t

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redu

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oruse

gammaradiation(effecton

material

strength?)

Pack“clean

”an

dbake.D

ebrisingresspreven

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material.

Airbags

Steriliz

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deploymen

t

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redu

ceou

tgassing.

Packan

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gammaradiation(effecton

material

strength?)

Ensure

insidesaresterilizeddu

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expo

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ondeflation.M

aterialdegradation?

Pack“clean

”an

dbake.D

ebrisingressredu

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ofairbag

material.Small(tolerated)

risk

offibers

beingpresen

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ndthelander

overcomeby

mod

ificationto

scientificmethod

.EDLS

/structure

Maintenan

ceof

sterility

after

assembly

Use

biosealan

dHEPAfilter

onthevent

Use

biosealan

dHEPAfilter

onthevent.

Frontshield

Presence

oforganismson

the

external

surfaces

Baketo

redu

cebioload(isthereahigh-

temperature

bake

duringman

ufacturingthat

will

redu

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bioload?)Maintenan

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AIV

andlaunch?

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sterility

(>50

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dryheat;rely

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13.4 Astrobiology Exploratory Missions of Concern to Planetary Protection 381

Hardw

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,con

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13 Astrobiology Exploratory Missions and Planetary Protection Requirements382

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13.4.2.3 Landers or Rovers with Martian Samples Returned to the EarthThe long-term strategy of the European Space Exploration Program foresees aMars Sample Return (MSR) mission as the most likely successor to ExoMars (seeChapter 12), and it is anticipated that in the future NASA and other space-faringnations will be interested in returning samples from Mars for in-depth scientificinvestigations.A Mars sample return mission falls into category V as “restricted Earth return,”

which means that the samples brought from Mars to the Earth need specialattention from the moment of collecting, through transport to Earth, and uponlanding on Earth. After arriving on our surface, it has to be proven that there is nobiohazard risk from the Martian samples. Even if there is only a remote possibilitythat the samples will contain specimens of microorganisms from Mars in a viablestate, Martian soil, rocks, or atmosphere must be kept under strong containmentaccording to the international treaty.Although a joint team of American and French scientists, provided by NASA and

the Centre National d’Etude Spatiale (CNES), working in the frame of a prelimi-nary design of a common Mars sample return mission has already defined apreliminary biohazard assessment test protocol for samples returned from Mars,a similar protocol still needs to be developed and adopted by ESA.In simple terms, the sample return container must meet the following require-

ments:• preventing back-contamination, and• preserving the integrity and the properties of the samples.

To avoid cross-contamination, the container must be hermetically sealed by meansof a mechanical system. Otherwise, the samples may be recontaminated byterrestrial compounds during the Earth atmosphere entry phase. Different meth-ods are envisaged to control the sealing before the release of the container systeminto Earth’s atmosphere:

• Determination by gas chromatography–mass spectrometry(GC-MS) of the leak rate by outside detection of a character-istic gas, e.g., helium or CO2 from the Martian atmosphere.

• If an atmospheric sample is collected, monitoring of thepressure inside the container – corrected by temperaturevariations – during cruise phase.

However, it must be recognized that each of these methods has its limits. A furtherrequirement is bio-cleanliness and sterility of the container; otherwise, care mustbe taken that the outside surfaces of the container are never in contact with theextraterrestrial environment. Before release into Earth’s atmosphere, three bio-logical barriers are required in order to comply with World Health Organizationrecommendations for the transport of hazardous biological material. Even in thecase of a non-nominal Earth return event, (in the worst case a crash or an uninten-tional landing in the sea), the container must maintain its hermetic seal and mustbe recovered.

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As a next step, a Mars Sample Receiving Facility (MSRF) must be available tohost the returned container and its content. Within this facility the material will beunpacked and analyzed accordingly to the defined scientific methods and stand-ards in the biohazard assessment protocol. This MSRF, which must provide a veryhigh degree of containment, must also prevent additional contamination of thesamples from Earth-bound inorganic, organic, or biological material. To theauthors’ knowledge, no such facility exists today that meets all these requirements.In order to formulate clear requirements for the MSRF, a functional project

definition must be provided. This requires interactive involvement of severalcommunities:

• the scientific community, in order to review and refineexisting draft test protocols that define the requirements ofthe instruments and methods;

• experts in containment technologies, in order to work out afunctional technical description of the high containmentfacility, resulting in a definition of space needs, technicalinstallations, and cost estimation, as accurately as possible;

• a team providing a thorough risk assessment for the wholetransport, including the way fromMars to Earth, the way fromthe landing site to the MSRF, and the work inside the facility;

• a group defining the research needs from the perspective ofdecontamination and sterilization of known Earth-bound andunknown Mars-bound life forms.

The starting point for the definition of a MSRF will be existing concepts of highcontainment and the necessary equipment, which exist on Earth mainly forbiosafety reasons.

Existing Concepts of High Containment Organisms are currently classified intofour risk groups: RG1 to RG4. Accordingly, there are also four biosafety levels:BSL1 to BSL4. (Note that there is no universally accepted standard for containment.BSL is the most widely used, so we have adopted it here.) For BSL4 laboratories,two distinct concepts exist, as follows:

• The cabinet laboratory, where all handling of the agent isperformed in a class III biological safety cabinet (BSC), whichis discussed later. The cabinet laboratory is arranged to en-sure passage through a minimum of two doors prior toentering any room containing the class III BSC.

• The suit laboratory, where the personnel wear a protective suit.The use of class II BSC cabinets is common in the suitlaboratory. (A suit laboratory was depicted in the movie Out-break, starring Dustin Hoffman, who portrayed an Armymedical expert sent to combat a deadly virus that destroyed asmall town in California and threatened the world.) With thispublicity event, suit laboratories became very popular and

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many new ones are currently being built. The BSL4 contain-ment zone should be located in a separate building or sealedroomwith independent air supply and exhaust systems. Theseair systems and components need to be sealed airtight and beaccessible from outside the containment area. A ventilatedairlock is required for the separation of higher and lowercontainment areas. The airlock is to have interlocking pneu-matic or compressible sealed doors with manual overrides.The personnel working in the suit laboratory wear a one-piece,positive-pressure suit that is ventilated by a life-support systemprotected by HEPA filtration (see below). The life-supportsystem includes redundant breathing air compressors, alarms,and emergency backup air tanks. A chemical shower is pro-vided to decontaminate the surface of the suit before theworker leaves the area. An emergency power source is pro-vided for the exhaust system, life-support systems, alarms,lighting, entry and exit controls, and BSCs. The air pressurewithin the personnel suit is positive to the surrounding labo-ratory. The air pressure within the suit area is lower than thatof the adjacent area. The entry to the containment area isequipped with magnetic gauges or pressure-monitoring devi-ces to prove directional flow. The containment area isequipped with audible alarms to detect depressurization.Supply air to the cabinet room or suit area and associateddecontamination shower and airlock is protected by passagethrough a HEPA filter. The exhaust of the laboratory’s suitarea, decontamination shower, and decontamination airlock istreated by passage through twoHEPA filters in a series prior todischarge to the outside. Redundant supply fans are recom-mended, and redundant exhaust fans are required.

HEPA Filtration The development of the HEPA filter during World War II wascritical for providing the necessary containment in the modern biosafety labora-tory. These filters are constructed of fiberglass “paper” that is pleated to maximizethe surface area of the filter, and they have a minimum particulate removal of99.97% for particles of 0.3 �m. The randomly oriented microfibers cause theparticles in the air stream to move in a circuitous path, forcing even the smallestparticles to collide with and adhere to the filter. The filter housings on contami-nated exhaust streams should be constructed to facilitate decontamination orshould be of the bag-in-bag-out design. Three glove sleeves are provided in eachbag to facilitate the handling of the filter during exchange.

Biological Safety Cabinets The biological safety cabinet (BSC) design has come along way since inception, with three main classifications: class I, class II, andclass III.

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Class I cabinets are defined as ventilated cabinets for personnel and environ-mental protection, with unrecirculated airflow away from the operator. Class Icabinets have a similar airflow pattern to a fume hood, except that the class Icabinet has a HEPA filter at the exhaust outlet, and it may or may not be connectedto an exhaust duct system. Class I cabinets are suitable for work with agents thatrequire BSL 1 or 2 containment.Class II cabinets are ventilated cabinets having an open front with inward airflow

for personnel protection, downward HEPA-filtered laminar flow for product pro-tection, and HEPA-filtered exhaust airflow for environmental protection. Class IIcabinets are suitable for work with agents that require BSL 1, 2, or 3 containment.Class II cabinets are differentiated into various types based on their construction,

air velocities, patterns, and exhaust system. For instance, class II type A cabinetsmay have contaminated plenums under positive pressure that are exposed to theroom, while class II type B cabinets must surround all contaminated positive-pressure plenums with negative-pressure ductwork. Type A cabinets can be ex-hausted into the lab or outside by way of a canopy connection, whereas type Bcabinets must have a dedicated, sealed exhaust system with remote blower andappropriate alarm system.Class III cabinets are totally enclosed and ventilated of gas-tight construction.

Operations are conducted through attached rubber gloves. The cabinet is main-tained under negative air pressure of at least 125 Pa. Supply air is drawn into thecabinet through HEPA filters. The exhaust air is treated by double HEPA filtration.The cabinet also has a transfer chamber capable of sterilizing workmaterials beforeexiting the glove box containment system. Class III cabinets are suitable for workwith agents that require BSL 1, 2, 3, or 4 containment.A typical cabinet laboratory, as required for a MSRL, would be composed of a

number of interconnected class III BSCs. All operations and handling would beperformed within the modules, which could in addition be of the double-wallcontainment type. The double-wall containment module would be of the box-in-the-box type with an inter-space surrounding a standard single-wall containment.This space would be at negative pressure relative to that of the room and the innercabinet in order to protect the personnel as well as to keep the sample pristine. If aMars-like atmosphere is required inside the module, an inert gas, such as nitrogen,could be fed to the module or a Mars-analogue atmosphere. For this reason, glovesand glove material have to be evaluated very carefully. Material transfer in and outof the modules and the containment would need to maintain confinement and thepristine nature of the samples. Different methods are in use today in laboratoriesworking with dangerous viruses.

Use of Robotics It might be necessary to include a robotics concept into thedesign of the MSRL in order to fulfill the requirements for non-contamination ofthe Mars samples by Earth-bound material. This could be for the whole spectrumof activities, including preparing, analyzing, and housing of samples, or it could befor single critical functions only, such as fine-scale manipulations to handle verysmall samples. It is not believed that existing robots from industrial applications

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could be used without further development. For obvious reasons, all the robotswould have to be of the type suitable for clean-room operation, and ISO class1–certified robots are now available. Aside from robot operations, class 1 certifi-cation is used in the semiconductor and pharmaceutical industries for achievingmini-containment environments.In conclusion, from the above arguments, it is clear that for design and con-

struction of a facility for Mars samples, new concepts and ideas are needed.Therefore, a program of research in high containment technology, in decontami-nation methods, and in material compatibility must be initiated well beforehand. Itis estimated that on the order of 10 years preparation is required ahead of samplearrival.

13.4.2.4 Human Missions to MarsA human mission to Mars has been a long-term goal in every space explorationprogram since the advent of space flight. Although any human endeavor to visit thered planet is still decades away, the implications of planetary protection require-ments on system development and mission operation in combination with thelong lead-time for the development of man-rated systems make this topic verytimely. A detailed understanding of these aspects is also necessary in order todefine the right robotic precursor missions to support the development of a humanmission scenario for Mars.It is not possible for all human-associated processes andmission operations to be

conducted within entirely closed systems. Therefore, a humanmission to Mars willcontaminate the planet to a certain extent. However, this forward contaminationcan and must be minimized by using appropriate procedures. In order to definethese procedures, we need to establish a better understanding of both the Martianenvironment and the fate of terrestrial contamination, particularly biological con-tamination, on this environment. Included in this context is the need for contain-ment or sterilization of solid, liquid, and gaseous waste products during surfaceoperations on Mars. Prior to leaving the surface, decontamination or stabilizationof the surface elements with respect to biological contamination will be necessary.The philosophy for backward contamination prevention is to break the chain of

contact betweenMars and Earth. Any contamination of the crew habitat onMars bypotential biological agents of Martian origin has to be avoided, as this contami-nation would be transferred to the crew and hence to Earth. Strict isolation of thecrew upon return is not practicable and would be difficult to implement. Twospecific issues are worth mentioning in this respect: the need for sophisticated dustmanagement and the need for emergency decontamination procedures for thesurface elements in case a contamination event takes place. The latter is simply atechnology adaptation based on already-existing systems. Dust management, how-ever, will be a challenging enterprise. The Apollo missions have already shown usthat dust can be a major problem when not managed properly. It can effectmechanical systems and endanger the health of the crew, independent of itschemistry. In addition, dust is a potential carrier of reactive chemical agents

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and, potentially, biological entities. A well-developed dust management systemrequired in order to implement effective backward planetary protection guidelinescan therefore also reduce the threat to crew health and safety. One aspect that willneed further reflection is the use of in situ resource utilization systems to produceconsumables for the crew.In summary, the planetary protection guidelines to limit contamination of Mars

and to avoid contamination of the Earth by potential Martian life will not be relaxedto accommodate a human mission to Mars. There are, however, two issues that arevery specific to a human mission to Mars. Regarding forward contamination, thebiological contamination of the spacecraft will increase during the mission becauseof the presence of the crew. For robotic spacecraft the bioburden limit set forth inthe planetary protection requirements has to be met at launch. The second, andcertainly not less important, aspect is that general human factors have to beconsidered along with planetary protection issues for a human mission to Mars.Critical elements of forward and backward contamination control depending onprocedures have to be designed in a way that makes them effective even in case ofhuman error.Although earlier human missions have a greater perceived risk, planetary

protection requirements likely will not become more relaxed in subsequent mis-sions. The main reason for this is that every mission will explore locations on Marsof high scientific (including astrobiological) interest that have not been visitedbefore.

13.4.3Missions to Venus

The current atmospheric environment on the surface of Venus, with an averagesurface temperature of 464 �C, is too hostile to support life, although the possibilityof the production of organic compounds in its atmosphere, e.g., by lightning, hasbeen suggested. Little is known about its history despite more than 20 probes sentto Venus since 1961 (see also Chapter 8). This lack of knowledge is due mainly toVenus’s high surface temperature, high pressure (95 000 hPa), and permanentthick clouds – primarily composed of aqueous solutions of H2SO4 – which obstructits exploration. It is assumed that in its early history Venus might have possessed asizable inventory of water and a cooler climate (100–200�C). Runaway greenhouseconditions that still exist today would then have led to evaporation of the water, itsphotolysis at higher altitudes, and escape of hydrogen. Today only traces of waterremain in the atmosphere of Venus. Owing to the high temperature at the surface,the lack of water, and the presence of toxic chemicals such as sulfuric acid,indigenous biological activity on or below Venus’s surface seems to be veryunlikely. The same is valid for the clouds, where temperature and pressure aremore moderate than on the surface but where drops of concentrated sulfuric acidprevail. However, Venus may have been considerably more Earth-like in its past,and thus it cannot be excluded that early environmental conditions on Venusmight have been favorable for the emergence and early evolution of life.

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Venus’s present environment not only is inimical to life but also makes heavydemands on the robustness of the technical equipment landing on its surface. Thefirst successful landing on the surface of Venus was achieved in 1970 with theSoviet Venera 7 mission; the landing probe survived the heat and pressure for23 min. This was followed in 1985 by the Soviet Vega 1 and Vega 2 twin missions,when the landers carried out surface studies for about 1 h. This environmentwould have killed any terrestrial microorganisms that might have traveled as blindpassengers with the lander from Earth to Venus.Venus is now being explored further by the European orbiter VenusExpress,

which entered orbit around Venus on 11 April 2006. NASA’s strategic explorationplans currently foresee the Venus In Situ Explorer and the Venus Surface Explorer tolaunch within the next decades.The COSPAR Planetary Protection Guidelines categorize all missions towards

Venus, whether orbiters, flybys, or landers, in category I. This infers that Venus isnot of direct interest for understanding the processes of chemical evolution and theorigin of life. Therefore, no planetary protection requirements are imposed. How-ever, NASA and a recent study by the U. S. Space Studies Board of the NationalAcademy of Sciences group all Venus missions, including sample return missions,into category II. This category applies to missions to celestial bodies that are ofinterest to astrobiology with regard to chemical evolution and the origin of life butpose only a remote risk of forward contamination by terrestrial microorganismsthat would jeopardize future exploration. The Space Studies Board study evenassumes that samples from the clouds or the surface of Venus would not raise asignificant backward contamination risk to the inhabitants of Earth.

13.4.4Missions to the Moons of the Giant Planets

Saturn’s largest moon Titan (see Chapter 9), Jupiter’s moon Europa (see Chap-ter 10), and probably also some of the other moons of the giant planets (see Chapter9) are of special interest to astrobiology; therefore, missions to these moons needspecial consideration from a planetary protection point of view. Their relevance toplanetary protection has already influenced the fate of the Galileo spacecraft, whichexplored Jupiter and itsmoons Io and Europa; at the end of its lifetime, in September2003, it was deliberately steered into the gravitational pull of Jupiter to avoidaccidental collision with – and possible contamination of – one of Jupiter’s moons.The surface of Titan was visited for the first time in 2005 by the European

Huygens probe of the joint NASA–ESA Cassini–Huygens mission to the Saturnsystem (see Chapter 9).Jupiter’s moon Europa is considered to be potentially habitable for indigenous

life (see Chapter 10). More than 95% of the spectroscopically detectable material onits surface is H2O. It has been established with high probability that this moon ofJupiter harbors an ocean of liquid water beneath a thick ice crust. In addition toliquid water, carbon and energy sources are required to support life as we know iton Earth. If carbon might have been delivered by impacts of various bodies

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(although crust resurfacing does not show very many impact craters), the questionof energy sources is still open. The existence of liquid water beneath the ice crustmay be the result of deep hydrothermal activity, radioactive decay, and/or tidalheating. In this case, conditions allowing prokaryotic-like life as we know it onEarth would have been gathered.NASA’s strategic exploration plan contains two missions to Jupiter’s moon

Europa: the Europa Geophysical Explorer in 2015 and the Europa AstrobiologicalLander well after 2030. Although it is premature to conclude that either an ocean orbiota exists on Europa, it is prudent to implement planetary protection proceduresthat assume the existence of both. Given the capabilities of terrestrial life to adapt toextreme conditions – such as heat, cold, pressure, salinity, acidity, dryness, andhigh radiation levels as well as combinations of these (see Chapter 5) – a con-servative approach needs to be taken to protect the Europan environment. Proper-ties of the Europan environment may present a target for contamination byterrestrial organisms carried on a spacecraft, which could colonize the entiremoon via a subsurface ocean connection. Whereas the COSPAR Planetary Pro-tection Guidelines classify orbiter and flyby missions to Europa as category IIImissions, the U. S. Space Studies Board, in the report “Preventing the ForwardContamination of Europa,” as well as an International Expert Group at a COSPAR/IAU Workshop on Planetary Protection in 2002 recommended classifying allmissions to Europa – including orbiters, landers, and penetrators – ascategory IV missions. This recommendation is based on the consideration thatorbiting spacecraft have a significant probability of ultimately impacting on thesurface. Any spacecraft component that is buried within the ice is effectivelyshielded from lethal levels of radiation, potentially allowing the survival of somecontaminating organisms. Episodic resurfacing of the young Europan crust couldthen bring spacecraft components in contact with the ocean.It was recommended that the bioload on spacecraft sent to Europa must be

reduced to such a level that the probability of inadvertent contamination of itsocean is extremely low (10–4 per mission). Further studies are needed in order todetermine

• the level of probability of survival and growth of terrestrialmicroorganisms in the Europan ice and ocean;

• methods of reducing the uncertainty in long-term survival ofmicroorganisms in the Europan surface/near-surface envi-ronment and in the turnover time of Europa’s icy crust; and

• the level of acceptable bioburden required for all parts of thespacecraft before launching.

13.4.5Missions to Asteroids or Comets

Small bodies in the Solar System (asteroids and comets) represent a very large classof different types of objects. Imposing blanket forward-contamination controls onthese missions seems not to be warranted. Currently, most such missions are

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classified as category I or II missions. Because such missions to comets andasteroids may become quite frequent in the future, further elaboration of therequirements may be needed.Comets in particular are of interest to astrobiology, because among all celestial

bodies, they contain the largest amount of organic molecules. They are consideredthe most pristine Solar System targets, bearing witness to the existence of adynamic organic chemistry from the earliest stages of our Solar System (seeChapter 2). Therefore, comets have been the target of several recent missions,whether as a flyby (European Giotto mission to comet Halley), by collecting andreturning samples of cometary dust from the tail (NASA Stardustmission to cometWild 2), by creating a crater on its surface by sending a 350-kg copper projectile intoa comet (NASA Deep Impact mission to comet 9P/Tempel 1), or by landing on acomet (ESA Rosetta mission to comet 67P/Churyumov-Gerasimenko).The Rosettamission, launched on 2March 2004, includes an orbiter and a lander.

After swing-by maneuvers at Earth (March 2005, November 2007, and November2009) and Mars (February 2007) and asteroid flybys at Steins (2008) and Lutetia(2010), it will reach the target comet 67P/Churyumov-Gerasimenko in 2014. TheCOSPAR Planetary Protection Guidelines require different considerations at dif-ferent mission phases:

• category III for the Mars gravity assist, which will bring thespacecraft as close as about 200 km to Mars, and

• category II for the comet exploration phase.

To meet the requirements of these categories, measures were taken to ensure verylow probability of impact at Mars and control of organic contamination on thecomet. Although the requirements of category II for the lander are less stringent,many measures and precautions were taken in order to control organic contami-nation and to avoid any confusion with regard to the results of onboard experi-ments searching for organic compounds and their precursors. This is an examplewhere the requirements of the experiments are more stringent than those set bythe COSPAR categorization. To meet the experiment requirements, the followingmeasures were taken:

• The whole system was integrated in a class 100 000 cleanroom.

• All organic materials (list, nature, references, and amount)in the project Declared Material List handled by ProductAssurance management were identified.

• At the design level, contamination sources were limited orcontrolled as far as possible, and the most possible contam-inant coming from various sources (such as out-gassing, gasleaks, organic material pollution, or abrasion during lander orexperiment operations, particularly drilling) or coming fromthe lander hardware was identified.

• Sensitive instrument parts were assembled in a class 100 or1 000 clean room and were cleaned with specific detergents

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and self-protection. Spectrometers were subject to purgingand sealing, and some of them will perform an initial blanknoise measurement in order to detect its internal contami-nation from terrestrial origin.

Japan’s asteroid sample return mission Hayabusa (MUSES-C) aimed at collectingpieces from asteroid Itokawa and then bringing the samples back to Earth. It isplanned that the sample return capsule will detach from the spacecraft and plungethrough Earth’s atmosphere for an intense reentry, with temperatures 30 timesgreater than those experienced by Apollo spacecraft. After reentry, the containershould parachute to Earth, where it can be brought to a laboratory for study. Althoughthe sampling of asteroid pieces has failed so far, this mission is of interest from thepoint of view of planetary protection. In view of the target comet type, theHayabusamission was classified as a category V mission with unrestricted Earth return.

13.5Outlook: Future Tasks of Planetary Protection

After the first formulation of COSPAR Planetary Quarantine Objectives in 1969,which were targeted mainly towards missions to Mars and other planets, it wasassumed that the question of indigenous life on the planets in consideration wouldbe solved within 20 years, a period assumed to encompass about 100 exploratory-type missions. History has shown this to be an overoptimistic assessment, and itdemonstrates that exploratory missions are influenced by a variety of parametersthat are not in the hands of space scientists but are largely dependent on politicsand economics.Although the missions so far sent to Mars, Venus, Titan, and comets have

provided a wealth of information on the habitability of the planets and theirrelevance for studies of chemical evolution and/or the conditions for origin andevolution of life, it will be the next generation of spacecraft that are targeted towardsin situ search for signatures of extant or extinct life forms. The European landerExoMars, to be sent to Mars in 2013, will be a prominent representative of thoseastrobiology missions (see Chapter 12). The COSPAR Planetary Protection Guide-lines already sufficiently cover such missions of high astrobiology relevance look-ing for putative life forms on Mars. They are all classified as either category IVb orIVc missions.Concerning Mars, future missions designed to bring planetary material back to

Earth – such as Martian rocks, dust, or atmospheric samples – are classified ascategory V missions with restricted Earth return. For those missions, detailedprotocols for sampling and sample handling and analysis to prevent both forwardand backward contamination are under development and eventually need to beadopted by COSPAR.A major task in view of planetary protection issues will be a mission sending

humans to Mars, which is part of the strategic long-term planning of both ESA and

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NASA. Activities associated with such human exploratory missions will interfacewith the terrestrial and extraterrestrial environment in three ways:

• The mission needs to be protected from the natural envi-ronmental elements of interplanetary space and the planetthat can be harmful to human health, to the equipment, or tothe operations. The following environmental elements needto be considered in order to protect humans and the equip-ment during their mission: cosmic ionizing radiation, solarparticle events, solar ultraviolet radiation, reduced gravity,thin atmosphere, extremes in temperatures and their fluctu-ations, surface dust, and impacts by meteorites and micro-meteorites.

• The specific natural environment of Mars should be protectedso that it retains its value for scientific and other purposes. Inorder to protect the planetary environment, the requirementsfor planetary protection as adopted by COSPAR for landermissions need to be revised in view of human presence on theplanet. Landers carrying equipment for astrobiological in-vestigations require special consideration to reduce contam-ination by terrestrial microorganisms and organic matter tothe greatest feasible extent. Records of human activities onthe planet’s surface should be maintained in sufficient detailthat future scientific experimenters can determine whetherenvironmental modifications have resulted from those ex-plorations.

• The Earth and its biosphere need to be protected from po-tentially harmful agents brought back upon return of theexplorers to their home planet Earth.

ESA, within its HUMEX study “Critical Issues in Connection with Human Ex-ploratory Missions,” has developed a roadmap identifying the research required toensure astronauts’ health and well-being during such a mission (Fig. 13.5).Finally, the question arises whether the increasing robotic exploration of Mars

and the eventual human exploration and settlement of that planet are likely tocause an environmental impact to scientifically important sites, regions of naturalbeauty, and historically important regions in the form of contamination withspacecraft parts and microbiota. The presence of crashed robots on Mars alreadyraises important questions about the type of wilderness ethic one may apply toMars and how this ethic is embodied within practical environmental policy.The environmental ethics that underpin a system of preservation/conservation

on the surface of other planets, such as Mars, have their origins in the “wilderness”debate, and therefore efforts for the protection of wilderness areas on Earth mightbe taken as an example. Anthropocentric reasons for declaring “natural parks”include the instrumental value of wilderness areas as sites for scientific study/preservation, human enjoyment, and the preservation of these regions for future

13.5 Outlook: Future Tasks of Planetary Protection 393

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human enjoyment. However, even in the absence of humans, non-anthropocentricreasons – such as the intrinsic value of the Martian landscape and potential dutiesto indigenous microorganisms, if they are there – still exist and can drive policyeven prior to human exploration. It is assumed that under the auspices of COSPAR(in addition to the current planetary protection policy, which is merely based on thescientific interpretation of the Outer Space Treaty), recommendations on how todeal with these ethical issues will be elaborated.

13.6Further Reading

United Nations. Treaty on Principles Governingthe Activities of States in the Exploration andUse of Outer Space, including the Moon and

Other Celestial Bodies (the “Outer SpaceTreaty”) referenced 610 UNTS 205 – reso-lution 2222(XXI) of December 1966.

13 Astrobiology Exploratory Missions and Planetary Protection Requirements394

Fig. 13.5 Roadmap of steps regarding human-health issuesrequired before a human mission to Mars takes place, asrecommended in the HUMEX study in the frame of ESA’sexploration program.

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13.6.1Concerning COSPAR Planetary Protection Guidelines

COSPAR Planetary Protection Guidelines:http://www.cosparhq.org/scistr/PPPoli-cy.htm

DeVincenzi, D. L., Stabekis, P. D. Barengoltz, JB. Proposed new policy for planetary pro-tection. Adv. Space Res. 1983, 3, 13–21.

DeVincenzi, D. L., Stabekis, P. D., Barengoltz,J. B. Refinement of planetary protectionpolicy for Mars missions. Adv. Space Res.1996, 18, 311–316.

Rummel, J. D. Report of COSPAR/IAU Work-shop on Planetary Protection, Williamsburg,VA, USA, 2–4 April 2002. 2002, available athttp://www.cosparhq.org/scistr/ppp.htm.

Rummel, J. D. Planetary exploration in thetime of astrobiology: protecting against bio-logical contamination. Proc. Natl. Acad. Sci.2001, 98, 2128–2131.

Rummel, J. D., Stabekis, P. D., DeVincenzi,D. L., Barengoltz, J. B. COSPAR’s planetaryprotection policy; a consolidated draft Adv.Space Res. 2002, 30, 1567–1571.

Rummel, J. D., Billings, L. Issues in planetaryprotection; history, policy and prospects,COSPAR Information Bulletin 2004, 160, 31.

Rummel, J. D., Billings, L. Issues in planetaryprotection: policy, protocol and implemen-tation, Space Policy 2004, 20, 49–54.

13.6 Further Reading 395

13.6.2Concerning Handbooks and Standards on Planetary Protection

CNES, System Safety. Planetary Protection Re-quirements. R�f�renciel Normatif, CNESRNC–CNES-R-14 (Edition 4)December 2002.

Debus, A. and the working group on ECSS,European standard on planetary protectionrequirements, Res. Microbiol. 2006, 157,13–18.

NASA, NASA Standard Procedures for theMicrobial Examination of Space Hardware,NPR 5340.1B, NASA, Washington DC.1980.

NASA; Planetary Protection Provisions forRobotic Extraterrestrial Missions, NPR 802012C; NASA, Washington DC. 2005

13.6.3Concerning Bioload of Spacecraft

Debus, A., Auburtin, T., Darbord J. C., Hydro-gen peroxide gas plasma sterilization proc-ess qualification for space application, SAEpublication ICES-128, 2000.

La Duc, M. T., Nicholson, W., Kern, R., Ven-kateswaran, K. Microbial characterization ofthe Mars Odyssey spacecraft and its encap-sulating facility. Environ. Microbiol. 2003, 6,977–985.

La Duc, M. T., Satomi, M., Venkateswaran, K.Bacillus odysseyi sp. nov., a round-spore-forming bacillus isolated from the MarsOdyssey spacecraft. Intern. J. System. Evolut.Microbiol. 2004, 54, 195–201.

Link, L., Sawyer, J., Venkateswaran, K., Nich-olson, W. Extreme spore UV resistance ofBacillus pumilus isolates obtained from anultraclean spacecraft assembly facility,

Microbial Ecology 2003, DOI: 10.1007/s00248–003–1029–4 [online].

Nellen, J., Rettberg, P., Horneck, G., Streit,W. R. Planetary protection – Approachinguncultivable microorganisms, Adv. SpaceRes. 2006, 38, 1266–1270.

Newcombe, D.A., Schuerger, A. Benardini, J. N.,Dickinson, D. and Venkateswaran, K. 2004.Survival of spacecraft associated microbesunder simulated Martian UV irradiation.Appl. Environ. Microbiol. 2005, 71, 8147–8156.

Nicholson, W. L., Munakata, N., Horneck, G.,Melosh, H. J., Setlow, P. Resistance of Ba-cillus endospores to extreme terrestrial andextraterrestrial environments. Microb.Molecular Biol. Rev. 2000, 64, 548–572.

Puleo, J. R., Fields, N. D., Bergstrom, S. L.,Oxborrow, G. S., Stabekis, P. D., Koukol,

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R. Microbiological profiles of the Vikingspacecraft.Appl. Environ. Microbiol. 1977, 33,379–384.

Rettberg, P., Horneck, G., Fritze, D., Verbarg,S., Stackebrandt, E., Kminek, G. Determi-nation of the microbial diversity of space-craft assembly facilities: first results of theproject MiDiv, Adv. Space Res. 2006, 38,1260–1265.

Schuerger, A. C., Mancinelli, R. L., Kern, R. G.,Rothschild, L. J., McKay, C. P. Survival of en-dospores of Bacillus subtilis on spacecraft sur-faces under simulatedmartian environments;implications for the forwards contaminationof Mars, Icarus 2003, 165, 253–276.

Venkateswaran, K., Satomi, M., Chung, S.,Kern, R., Koukol, R., Basic, C., White, D.Molecular microbial diversity of a spacecraftassembly facility. Syst. Appl. Microbiol. 2001,24, 311–320.

Venkateswaran, K., Kempf, M., Chen, F.,Satomi, M., Nicholson, W., and Kern. R.Bacillus nealsonii sp. nov., isolated from aspacecraft-assembly facility, whose sporesare gamma-radiation resistant. Int. J. Syst.Bacteriol. 2003, 53, 165–172.

Venkateswaran, K., Hattori, N., La Duc, M. T.,Kern, R. ATP as a biomarker of viable mi-croorganisms in clean-room facilities. J.Microbiol. Meth. 2003, 52, 367–377.

13 Astrobiology Exploratory Missions and Planetary Protection Requirements396

13.6.4Concerning Lunar Missions

Allton, J. H., Bagby, Jr. J. R., Stabekis, P. D.Lessons learned during Apollo lunar samplequarantine and sample curation. Adv. SpaceRes. 1998, 22, 373–382.

13.6.5Concerning Missions to Terrestrial Planets

Cockell, C., Horneck, G. A planetary park sys-tem for Mars, Space Policy 2004, 20, 291–295.

Debus, A., Runavot, J., Rogovski, G., Bogo-molov, V., Darbord J. C. Mars ’94/’96 mis-sion planetary protection program, techni-ques for sterilization and decontaminationlevel control, IAF-95-I.5.10. 1995.

Debus, A., Runavot, J., Rogovski, G., Bogo-molov, V., Khamidullina, N., Trofimov, V.Landers sterile integration. Example of Mars96 mission, Acta Astronaut. 2002, 50,385–392.

Debus A., Planetary protection requirementsfor orbiter and netlander of the CNES/NASA Mars sample return mission, Adv.Space Res. 2002, 30, 1607–1616.

Debus, A. Planetary protection: organisation,requirements and needs for future planetaryexploration missions, Proceedings of the 37th

ESLAB Symposium – Tools and Technologiesfor Future Planetary Exploration, ESA SP-543,ESA-ESTEC, Noordwijk, The Netherlands,pp 103–114, 2003.

ESA web site: http://sci.esa.int/science-e/www/area/index.cfm?fareaid=9#

ESA, Lessons Learned from the Planetary Protec-tion Activities on the Beagle 2 Spacecraft,Report Reference P3450026, ESA ESTEC,Noordwijk Holland, 2005.

Horneck, G., Facius, R., Reitz, G., Rettberg, P.,Baumstark-Khan, C., Gerzer, R. Crticialissues in connection with human missionsto Mars: protection of and from the Martianenvironment. Adv Space Res. 2003, 31, 87–95.

Horneck, G., Facius, R., Reichert, M., Rettberg,P., Seboldt, W., Manzey, D., Comet, B.,Maillet, A., Preiss, H., Schauer, L., Dussap,C. G., Poughon, L., Belyavin, A., Heer, M.,Reitz, G., Baumstark-Khan, C., Gerzer, R.HUMEX, a Study on the Survivability andAdaptation of Humans to Long-DurationExploratory Missions, ESA SP 1264. ESA-ESTEC, Noordwijk, 2003.

Kminek, G., Rummel, J. D. (Eds.), PlanetaryProtection – Human System Research and

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Technology, ESA-WPP-253, ESA-ESTEC,Noordwijk, 2006.

MEPAG Report: Findings of the Special RegionsScienceAnalysisGroup (Draft),MEPAGSpecialRegions Science Analysis Group, 2006; avail-able at http://mepag.jpl.nasa.gov/reports/

NASA web site: http://mars.jpl.nasa.gov/over-view/

Rummel, J. D., Race, M. S. A Draft Test Protocolfor Detecting possible Biohazards in MartianSamples Returned to Earth,NASA/CP -2002–211842, NASA, Washington D. C. 2002.

Sims, M. R. (Ed.) Beagle 2 Mission Report Uni-versity of Leicester UK, ISBN 1 898489 35 1,2004.

Space Studies Board of the U. S. National Re-search Council, Preventing the Forward Con-tamination of Mars, The National Academies

Press, Washington D. C. 2006, availableonline at http://fermat.nap.edu/catalog/11381.html

Space Studies Board of the US NationalResearch Council Assessment of PlanetaryProtection Requirements for Venus Mis-sions – Letter Report, 2006, available onlineat http://darwin.nap.edu/books/0309101506/html/3.html

Space Studies Board of the US NationalResearch Council, Safe on Mars, PrecursorMeasurements Necessary to Support HumanOperations on the Martian Surface, NationalAcademy Press, Washington D. C., 2002.

Lessons Learned from the Viking Planetary Quar-antine and Contamination Control Experience,Bionetics Corporation, contract NASW-4355.NASA, Washington D. C. 1990.

13.7 Questions for students 397

13.6.6Concerning Missions to Jupiter’s Moon Europa

Space Studies Board of the US National Re-search Council, Preventing the Forward Con-tamination of Europa, 2000, available onlineat http://www.nap.edu/openbook/NI000231/html/index.html

Planetary Protection and Contamination ControlTechnologies for Future Space Science Missions,Document D-31974, JPL/California Instituteof Technology, Pasadena, 2005.

13.7Questions for students

Question 13.1Describe the COSPAR Planetary Protection Guidelines, the rationale and re-

quirements for different missions within our Solar System.Question 13.2Develop a Planetary Protection Plan for a mission landing on a carbonaceous

asteroid.Question 13.3Describe the planetary protection requirements and implementation plans for a

robotic lander mission to Mars depending on the landing site and the purpose ofthe mission.Question 13.3Assess the impact of a human mission to Mars from the point of view of

astrobiology and planetary protection (pros and cons).Question 13.4Give reasons, other than scientific ones, for requiring protection of the planets of

our Solar System and justify them.

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Index

aacetonitrile 243acetylene 243, 247action spectroscopy 310action spectrum 306adaptation

– molecular 139adenine 92, 114

– synthesis 76–77adenosine 92aerogel collectors 305aerosols 235, 241, 243albedo 157ALH84001 16 ff., 329aliphatic hydrocarbon 98amino acid 5ff., , 24, 42, 49, 58, 108, 236, 323,

342– aspartic acid 305– b-amino isobutyric acid 5 ff., 86, 305– glutamic acid 305– synthesis 75

ammonia 24, 87, 228, 242, 246– hydrates 229

amphiphilic 97–98analytical laboratory 339Announcement of Flight Opportunity 302Antarctic dry valleys 333anti-greenhouse 241antigreenhouse 227Apollo 273, 303, 309, 312

– command module 374ff.– lunar module 375– lunar samples 375ff.

Apollo-Soyuz 312Archaea 88, 124–128, 265archaebacteria 124–125Archean rock 329, 330 ff.argon 242Ariane 5 338

aromatic hydrocarbon 98Arrhenius, Svante 307artificial meteorite 309, 313ASI 225asteroid 46–47, 390

– Hayabusa 392astrobiology experiments 303

– Low Earth orbit 286astrodynamics 179ff.astronomical unit 159asymmetrical carbon 60atmosphere 69, 85ff., 156, 227

– non-reducing 7atmospheric oxygen

– rise 157, 163ATP 100, 264ATPase 264attitude and orbit control system 199AURORA 326autocatalysis 14autotrophic 24

bBacillus pumilus 371Bacillus stearothermophilus 372Bacillus subtilis 309, 311, 313, 372

– spores 306, 310, 312Bacteria 88, 122, 124–128, 246, 265

– survival 121Barberton 15, 166, 172basalt 17Beagle 2 324, see also Marsbenzene 243, 245bioburden reduction 367

– biocleaning 370– isopropyl alcohol 371– surface wiping 371

– D value 371– Dry-heat sterilization 370, 372

399

Complete Course in Astrobiology. Edited by Gerda Horneck and Petra RettbergCopyright � 2007 WILEY-VCH Verlag GmbH & Co. KGaA, WeinheimISBN: 978-3-527-40660-9

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– gamma radiation sterilization 370, 371– H2O2 gas plasma sterilization 370, 372– sporicidal 371– Viking pre- and post-sterilization 369– Z value 371

bioload measurement– ATP bioluminescence assay 367– B. pumilus SAFR-032 365– B. subtilis 168 365– Bacillus group 366– Bacillus spore 364– colony-forming units (CFU) 363– culture-based microbial assay 363– fluorescence analysis 367– limulus amebocyte lysate assay 367– Live/Dead 367– Micrococcus 365– non-cultivable microorganisms 367– pasteurization 364– PCR 364, 367– rDNA 367– Staphylococcus 365– swabbing 363

bioload numbers 382biological safety cabinets 385biomarkers 329biomass 246, 305BIOPAN 10, 283, 305, 307, 309

– biological samples 288– environment

– microgravity 293– pressure sensor 292– radiation dosimetry 293– radiometer 292– solar electromagnetic radiation 292– temperature history 292– UV sensors 292

– experiment environment 287, 290– experiment hardware 285– experiments 286, 287– exposure experiments 282ff., 322– integration 288– lid 289– radiation level 287– sensors 285– simulated mission profile 288– temperature profile 287

biosafety levels 384bioshield 372biosignatures 329biosphere 87, 162, 306BIOSTACK method 311blank sample 344

bombardment 86branching ratios 231breakthrough organism 108brown dwarf 30 ff.building blocks 114ff.building blocks of life 86 ff.Butlerov, Alexandr 65

ccabinet laboratory 384carbodiimides 12carbohydrates 24carbon 32ff., 247, 264carbon chemistry in water 3 ff.carbon dioxide 41, 44, 47, 243

– removed from atmosphere 47carbon isotopes 5 ff.carbon monoxide 35, 38, 41ff., 48, 243carbonaceous chondrites 98carbonate-silicate cycle 157 ff.Cassini 324Cassini-Huygens 19, 225, 236, 245, 247–248,

323–324– ACP 240, 244– camera 224, 239– Cassini 224, 237–238, 241–242, 245,248–249

– CIRS 238, 243– DISR 239–241, 244, 245, 247– GC-MS 239–243, 245, 247– HASI 240– Huygens 237, 239–245, 247– INMS 238, 242– ISS 238, 248– radar 238, 249– SSP 239–240, 245– UVIS 238– VIMS 238, 248–249

catalysis 90category IV missions 362category V missions

– restricted Earth return 376cell 56

– communication 90– interaction with environment 118

Ceres 48charge [Z] 312chemical propellants 182chemical uncertainties 233chemiosmotic theory 160chemistry

– organic 223, 233, 245– prebiotic-like 55, 248

Index400

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chemolithoautotrophs 155, 161chloroplast 89, 103chondrites 45–46, 48, 50CHONSP 156chromosome 103circular polarization 8circularly polarized synchrotron radiation 8clay 6 ff., 99, 113, 116clay minerals 305clean room 368, 373, 378, 391clouds 241CNO cycle 32 ff.co-oligomers 236coat protein 107codon 94ff.cold plasma 234Columbus

– International Space Station 295Comas-Sola, Jos� 225comet missions

– Deep Impact 391– Giotto 391– Rosetta 391

Comet Hale-Bopp 9Comet Halley’s 9Comet Hyakutake 9Comet Shoemaker-Levy 9 9Comet Wild 2 305comets 8 ff., 46–47, 50, 71, 224, 390command and data handling 199communication system 199complex organics 244condensing agents 12conjugation 102conserved genes and sequences 99, 101contact instruments 339, see also ExoMarscontaminants 344cosmic radiation

– shielding 312cosmic rays 245COSPAR 355

– Panel on Planetary Protection 357COSPAR planetary protection guidelines

388, 391– backward contamination risk 389– category I 389, 391– category I missions 368, see alsoMercury, Venus

– category II 368, 389, 391– category II missions, see also Jupiter,Saturn

– category III 376 ff.– category III mission 390

– category III missions 362, 368, see alsoMars orbiters

– category IV 376ff.– category IV missions 368, 390, see alsoEuropa, Mars

– category IVa 378– category V 376ff., 383, 392– category V missions, see also safe forEarth return

– COSPAR planetary protectioncategories 358

– implementation of planetary protectionguidelines 362

– restricted for Earth return 361, 383– Viking lander post-sterilizationlevels 368, 379

– Viking pre-sterilization level 368cryobot 268crystalline physiology 6cyanamide 12cyanoacetylene 242–243cyanogen 242–243cyanopolyynes 231cyclobutadipyrimidines 310cyclobutane thymine dimers 311cytosine 60ff., 92, 114

– synthesis 78

dD-amino acids 5, 60, 126D/H ratio 49Darwin, Charles 2Darwin-Eigen cycle 106Darwin-IRSI 20Darwinian evolution 87decarboxylation 11Deinococcus radiodurans 145deoxyribonucleic acid 60deoxyribonucleotide 92, 105deoxyribose 92depth-dose distribution 315desiccation 146diacetylene 243dicyandiamide 12dicyanoacetylene 243dielectric constant 4diffusion coefficient 230dihydrogen 227dipole moment 4disk 45DNA 5ff., 23, 60, 91, 105, 310–311

– absorption characteristics 280

Index 401

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– damage to– DNA strand breaks 310

– junk-DNA 93– photoproducts 310

DNA genome 103DNA-protein crosslinking 311DNA-RNA-protein life 91, 105dolomite 17domains of life 88dosimetric systems 315double helix 116drill 335, 342 ff.dust 43dust particles 335

eearly Earth 314, 328early Mars 329early replication 110early solar nebula 305Earth 204–205, 208, 237, 241

– accretion 85– age 46– crust 85– early

– habitability 166– life 171

– formation 46– greenhouse effect 156– habitability criteria 165– habitats 165

Earth orbit 303Earth-Moon system 376Earth’s magnetic field 275ff.Earth’s obliquity 164Earthlike exoplanets 19eccentricity 227, 268ecological niche 88ecosystems

– endoevaporitic 313– endolithic 313

EETA 79001 16 ff.effective doses

– low Earth orbit missions 314– missions to the Moon 314

Eigen limit 106 ff.electrical power system 199electron acceptor 160, 264ff.electron donor 160, 264 ff.electron impact 234elements

– formation 25, 28–29ELIPS 326

emergence of life 304enantiomeric excesses 8enantiomers 60, 330endocytosis 102endogenous sources of organic molecules 69endolithic microbes 333endoparasites 100endospores 130, 364

– bacterial– resistance 147ff., 310

endosymbionts 103endosymbiotic 93energy conservation equation 187ff.energy sources 264ff.energy supply 155energy [E] 312environment habitable 155enzyme 87ff.ERA, see also EURECA

– exposure experiments 322erosion 86error threshold 106ESA 225, 281, 302, 304, 307, 313, 316, 321

– exploration program 317, 322ff.ethane 243, 246ethylene 243ethylene oxide 235eubacteria 124–125Eukarya 88, 125, 127eukaryotes 124–125

– size 123EURECA 280–281, 303, 308–309, 312

– Exobiology Radiation Assembly 304Europa 17, 155, 159, 223, 253ff., 307, 368–369

– core-ocean interface 267– cryovolcanic activity 257– density 258– evolution 253ff., 260– Galileo 389ff.– gravity potential 258ff.– ice crust 264, 266– internal structure 258– ionizing radiations 266– iron core 258, 260– life 263– magnetic field 258– ocean 154, 255, 266–267– raft model 256– rafts 255– silicate-ocean interface 256, 268– subsolidus convection model 257– surface features 255– thermal boundary layer 262

Index402

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– thermal convection models 262– tidal forces 255ff.– tidal heating 260– water ice 257, see also water– water ocean 258

European Astrobiology Network Association268

European Space Exploration Program 383evolution

– Darwinian evolution 87 ff.– molecular evolution 87 ff.

evolution of life 306exhaust velocity 182exobiology 321ff.exogenous delivery of organic molecules 71ExoMars 16, 339 ff., see also Mars

– access to subsurface 346ff.– Pasteur 316

ExoMars rover 327exoplanets 20EXPOSE 282, 305, 308, 313–314, 317

– Experiment Verification Test Program303

– exposure experiments 323– hardware 299– integration 301– sample carriers 299– sensor packages 316– Sun pointing devices 316– thermal conditions 316

EXPOSE experiments– EXPOSE-R 297

EXPOSE facility 365– bacterial cells or spores 296– engineering model 301– EXPOSE-E 295– EXPOSE-R 295, 297, 299– fern spores 296– fungal spores 296– International Space Station 295– plant seeds 296– sensors 296– telemetry/telecommands 297

EXPOSE-experiments– EXPOSE-E 297–298– EXPOSE-R 298

exposure experiments– BIOPAN 322– ERA 322– EXPOSE 323– STONE 323

exposure facilities 282extant life 332, 334 ff.

extinct life 328, 334 ff.extinction (of light) 36–41extrasolar life 20extrasolar planet 19 ff., 173extraterrestrial organic molecules 8extreme environments 121

– survival 129extremophiles 121 ff., 154, 266

– acidophilic 170– alkaliphile 129– applications 138– barophile 129, 140– define 121ff., 127– halophiles 127– hyperthermophile 129– piezophiles 140– psychrophile 129, 139– thermophiles 127

fF stars 37, 159fatty acid 11, 67, 98fermentation 162Fischer-Tropsch reactions 247, 265flow reactor 234folded proteins 94formaldehyde 7, 24, 41 ff., 49, 87fossil cyanobacteria 172Foton 281–282, 304–305, 307, 309, 314

– acceleration levels 284– BIOPAN 288, 291ff., see also BIOPAN– capsule reentry 290– descent module 283, 291, 294– heat shield 294– orbital parameters 291ff.

ggalactic cosmic radiation 311Galilean satellites 223–224, 253, 261, 265Galileo mission 18, 254–255, 257, 267

– magnetic and geodetic measurements258

– magnetometer 18– near-infrared mapping spectrometer(NIMS) 257

Ganymede 226, 253, 258gas chromatography-mass spectrometry 383Gemini 309gene

– gene transduction 102– gene transfer 102– gene transformation 102

gene products 90

Index 403

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genetic code 94, 105genetic information 88, 92, 103genetic takeover 6genome 103

– DNA genome 92, 103– RNA genome 103

genome length 106genotes 105geophysics and environment package (GEP)

327, 335 ff.geosynchronous orbit (GEO) 191geothermal fluid 99glycerol 13glycine 42glycoaldehyde 42gravity potential 268 ff.gravity-assist maneuver 193ff., 198Greenberg, J. M. 304greenhouse effect 85, 156, 158, 227, 241guanine 92, 114

– synthesis 77guanosine 92Gunflint Formation 172

hH into He 32H-bonding 4H2O 35, see also waterhabitability

– assessment– Age of Retreat 153– astrobiological gap 166– history 151ff.– period of optimism 152– Rebirth of Optimism 153

– energy 160– impact flux 164– Moon 164– postulate of 168, 173– temperature 156– test cases 169

habitable worlds– Earth 156, 208– uninhabited 156

habitable zone 30, 159– continuously habitable zone 160– liquid water 155

Haldane, John 65halite 121halite, extraterrestrial 143–144haloarchaea 140halobacteria 140Halococcus 141–142

hardware– experiment trays 299– EXPOSE 299– filters

– cutoff 299– neutral density 299

haze particles 227heavy bombardment 47helices 5helium 32ff., 42

– formation 25, 32HEPA filtration 385ff.Herschel, John 225Herschel, William 152Hertzsprung-Russell diagram 29ff.heterotrophy 161high temperature environments

– coal refuse piles 135– deep hydrothermal vents 70, 99, 135,255, 265

– Iceland 134– Italy 134– Yellowstone National Park 133ff.

high-salt environments– brines 140– rock salt 141

Hohmann transfer 190, 195, 197homochirality 4 ff., 97, 330Horsehead nebula 39HST 236Hubble constant 27human exploratory missions

– HUMEX study 393human mission to Mars

– human-health issues 394human phantoms 315Huygens, Christian 225hydrates 228hydrocarbon 42, see also aliphatic hydrocar-

bon, aromatic hydrocarbonhydrocarbons 24, 87, 235, 242, 245–246hydrogen 243, 304

– 21 cm line 37– formation 25– H 42– H2 37, 42–43, 47– HII 37, 44

hydrogen cyanide 7, 24, 42, 49, 87, 242–243hydrogen sulfide 8hydrolysis 113hydrolysis polymerization 116,

see also templated polymerizationhydrophilic 24, 97

Index404

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hydrophilic groups 4ff.hydrophobic 24, 97hydrophobic groups 4 ff.hydrothermal systems 7ff.hydrothermal vents 70, 99, 154, 255, 265, 266hydroxyapatite 12hyperthermophile

– acidophile 129HZE particle 311

– d-rays 312– thin-down effect 312

iice 41, 113

– eutectic 113ice shell 268icy satellites 268illite 12impact 85impact craters 256, 264inclination 227Infrared Space Observatory 18, 236, 243infrared spectra 304inorganic surfaces 99International Space Station (ISS) 274, 295,

301, 304–305, 315, 317, 323, 365– Columbus 302– European Columbus module 282, 295– EUTEF-CEPA (Columbus ExternalPlat-form Adapter) 296

– EUTEF-CEPA (I/F) 297– EXPOSE facility 295– MATROSHKA 315– outer platform EUTEF 302– Russian module 301, 315– Russian Zvezda module 282– temperature limits 281

interplanetary space– cosmic radiation 275– extreme temperatures 274– radiation field of solar and galacticorigin 274

– GCR 275ff.– microgravity 281– microgravity level 287– radiation belts 278– solar cosmic radiation 275– solar extraterrestrial UV 279– solar particle events 275– space vacuum 274, 280– temperature 280ff.

interplanetary transfer of life 307, 313interplanetary dust particles 305

interstellar absorption 37interstellar cloud

– collapse 29, 44– IR spectroscopy 38– radio spectroscopy 37

interstellar grains 8 ff., 43, 45, 304– formation 39 ff.– minerals 40– observed properties 40

interstellar ice 41interstellar matter 35interstellar medium 304interstellar molecular clouds 71interstellar molecules 38–39, 41–42, 53intervening sequences, see also introns 94introns 94Io 223, 253, 258ion gradient 98ionizing radiation 266, 335, 342ff.iron sulfide 8ISO 18, 236, 243isoform

– a-isoform 115– b-isoform 115– D-isoform 115– L-isoform 115

isoprenoid 98isotope 86isotope biosignatures 329isotope distribution 4isotopic fragmentation 247Isua Greenstone Belt 172

jJeans, James 29, 225Jeans’ mass 29Jupiter 46, 50 ff., 237, 253 ff.

kKepler, Johannes 185Kepler’s laws 185, 226kinetic constants 231kinetic data 233kinetic modeling 230Kuiper, Gerard Pieter 225Kuiper Belt objects 46, 53, 205, 214

lL-isoform 115laboratory simulations 229Lake Vostok 139Laplace resonance 268laser altimeter 268

Index 405

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Last Universal Common Ancestor (LUCA)96, see also LUCA

lateral gene transfer 101launch acceleration 181launch windows 195laws of motion 185LDEF 303, 305, 309, 313left-handed (L)-configuration, see also L-isoformlichens 309life 55, 117, 246–247

– boundaries 154– definition 3, 117, 263– elements 24– emergence 223– extrasolar 20– requirements 155, 265, 321– silicon-based 156

life beyond Earth 220life in a test tube 11life, interplanetary transfer 323life, liquid water 322 ff.lifetime of a planet 164linear energy transfer [LET] 312lipid 24, 90, 97, 128

– high temperature 127– pH extremes 127

lipid bilayers 97Long Duration Exposure Facility 305Lord Kelvin 307low Earth orbit (LEO) 179ff., 303–304

– experiments 273ff., 281low-energy transfer 196low-temperature environments 138low-thrust maneuvers 192Lowell, Percival 152LOX 182LUCA 96, 98, 100, 103Lucretius 152Lunar Receiving Laboratory 375ff.Lyman alpha 231–232, 234

mM stars 37, 159magma ocean 47magnetosphere 231, 234, 276–277Maillard reactions 309main sequence stars 35main sequences 30 ff.maneuvers 190ff.Mars 48, 50, 173, 208, 223, 307, 313–314, 368,

392– Mars ’96 mission 324, 332, 373– Beagle 2 372–373, 380–382

– biologically available nitrogen 167–168– canals 152– dry river beds 376– environmental ethics 393– evidence for water 210– evidence of heat 213– ExoMars 383, see also ExoMars

– access to subsurface 346ff.– extant Martian life 15ff., 368– habitability 159– human activities 317– human mission 387– life-detection experiment 368ff.– magnetic regions 158– Mariner 9 376– Mars Exploration Rovers 378ff., 382– Mars Express 359, 376 ff.– Mars Global Surveyor 359, 376 ff.– Mars Odyssey 15, 359, 376 ff.– Mars Pathfinder 373, 378 ff.– Mars Reconnaissance Orbiter 334, 359,376 ff.

– Mars sample return (MSR) 196, 198,316, 383

– Mars Sample Receiving Facility(MSRF) 384ff.

– robotics 386– sample return container 383

– Mars Science Laboratory 16, 379– MER 345ff., 382– meteorites from Mars 213, 308– microfossils in a martian meteorite218

– Opportunity 16, 378 ff.– past and present missions 377– past liquid water 152– Phoenix 379– plate tectonics 158– signatures of life on Mars 219– simulated Martian UV 365– simulated soil 309– special region 368– Spirit 378ff.– UV radiation climate 168, 307– Viking 130–132, 367–368, 382– Viking 1 378ff.– Viking 2 378ff.– Viking landers 372– volcanism 158

Mars exploration 316Mars Express 16, 324, 334Mars Mission 195Martian meteorite ALH84001 16 ff., 329

Index406

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Martian meteorites 308– atmospheric infall 294

MATROSHKA 315membrane 11, 24, 56

– bilayers 97– containment in 97

Mercury 44, 204–206mesosphere 241metabolism 246

– chemolithotrophic 155– heterotrophic 155, 161– photosynthesis 155

metal sulfide precipitate 99metamorphic processes 329metamorphosis 86meteorite flux 9meteorites 8 ff., 41, 45, 73, 224, 323

– landing 314meteoroids 322methane 24, 41, 49, 87, 225–227, 232, 234,

236, 243, 246–248methane hydrates 247methanol 41methylation 105Metrodorus of Chios 152microbial mats 172microfossils 14, 121–122

– cyanobacteria 172– morphology 329– yeasts 172

micrometeorites 47, 74, 305, 314– carbonaceous 9ff., 305

microorganisms 88, 122ff., 172, 174, 323microspheres 12Miller, Stanley 66, 233mineral 115MIR station 10, 305mitochondria 89, 103mobility 327, 345 ff.molecular crowding 93molecular evolution 87molecular properties

– DNA stability 136– halophiles 143– hyperthermophiles 136– lipids 136– proteins 136

molecules– first 35– precursor to life 24, 55ff.

montmorillonite 11, 13 ff.Moon 47–48

– Apollo missions 374ff., 387

– Surveyor 3 376Moon-forming inpact 46mRNA 94multicellular life 163multiple-staged rockets 183Murchison meteorite 8, 49, 305mutation 100, 106

– mutation rates 103

nNASA 3, 225–226, 305NASA’s strategic exploration plan 390Neptune 46, 50ff.neutron star 8, 34Newton’s laws 185, 194Newton’s universal law of gravitation 185nitriles 235nitrogen 34, 42, 47, 227–228, 242–243

– biologically available form 33ff., 167non-coding sequences 93nucleic acids 23, 323nucleoside 61, 92, 114

– b-orientation 114nucleosynthesis 32

– primordial 25nucleotide 49, 61, 86 ff.

– D-isoform 114–115, see also deoxyri-bonucleotide and ribonucleotide

nucleus 88 ff.nutrients 155

oobliquity 227ocean (on Europa) 229, 247oligomers 236one-handedness 4 ff.Oparin, Aleksandr Ivanovich 64Opportunity 16, see also Marsorbital mechanics 179 ff., 184organelle 89, 103organic molecules

– extraterrestrial 7 ff., 304origin of life 1 ff., 48–49, 63 ff., 86 ff.Orion cloud 39Orion nebula M42 35, 38 ff., 44Orion OMC-1 star 8osmotic potential 98Outer Space Treaty 354, 394oxidant 332, 335 ff., 342 ff.oxide 305oxidized 321oxidizers 182oxirane 235

Index 407

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oxygen 33ff., 42, 122, 139, 155–162, 172–173ozone hole 306ozone layer 314

pp-p chain reaction 32 ff.p-RNA 13paleobiologists 329panoramic instruments 339panspermia 307, 323

– entry process 308– escape process 308– interim state in space 308

parameters of space– effects 313

parasites 107Pasteur payload 327ff., see also ExoMarspasteurization 365payload 179ff.payload fraction 181, 192, 196peer review board 302peptide bond 58ff., 80, 96ff.peptide nucleic acids 14peptidoglycan 125, 126 ff.permafrost 138, 334permeability 98PERSEUS experiment 305phosphates 113phosphodiester bonds 113, 116photoautotrophs 161–162photochemical modeling 232photodissociation 234photolysis 11photoproducts 311

– DNA 310phylogenetic studies 101phylogenetic tree 88, 101, 124

– hyperthermophiles 137Pilbara 15, 172, 329Pioneer 11 226planet 85

– formation 44 ff.planetary nebula 33planetary protection 257, 307, 317, see also

COSPAR planetary protection guidelines– backward contamination 387– backward contamination prevention355

– concern of back-contamination 375– forward contamination prevention 355– Mobile Quarantine Facility 375– planetary protection guidelines 355ff.– planetary protection strategies 382

– preservation of the extraterrestrialsamples 355

– rationale for planetary protection 354ff.Planetary Protection Implementation Plan

362, 379, 381Planetary Protection Plan 362, 380planetary surface 158

– temperature 157planetesimal 45, 228, 242planets

– Earthlike 152– extrasolar 152

plasmids 102plate tectonics 329ploidy level 103PNA 14polarization 36polycyclic aromatic hydrocarbons (PAHs) 40,

43polymer 113, 236

– synthesis 80polymerization 113polypeptide 94, 96, 105polyynes 231pre-stellar evolution 304prebiotic chemistry 55 ff., 324prebiotic synthesis 114precursors 58, 114 ff.precursors of life 304pressure (on Titan) 227primordial atmosphere 248progenote 88, 105, 108Progress 301prokaryotes 88, 121, 124–125

– size 123propane 243propulsion system 199propyne 243protein 55–60, 63ff., 80, 96, 264

– catalytic protein 63ff., 87, 90, 105– genetically encoded 108– protein catalyst 103, 105, 110– protein domains 100– protein folding, see also protein struc-ture, protein domains

– protein strucutre 100– protein synthesis 110

– genetically, encoded 108, see alsotranslation

– regulatory proteins 107– scaffolding proteins 106, see also geneproducts

– structural protein 90, 106

Index408

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proteinoids 11proto-ribosome 109proton gradient 100protoplanetary disk 44 ff., 85protosolar disk 49purine 8, 57, 60–63, 81, 87, 114

– synthesis 76purine base adenine 60purine base guanine 60pyranosyl-RNA 13pyrimidine 8, 87, 114pyrimidine bases 76pyrimidine base cytosine 60pyrimidine base thymine 60(6–4) pyrimidine-pyrimidone adducts 310pyrite 8pyrophosphate 13

qquantum yield 231, 232

rracemic mixture 115, 330racemization 11radiation 286

– belts 278– SouthAtlanticAnomaly (SAA) 279

– cosmic radiation– dose equivalent 275– Gray 276– quality factor 275– Sievert (Sv) 275

– field of solar and galactic origin 274– galactic cosmic 275

– HZE particles 276– GCR 275– solar cosmic 275

– solar particles events (SPEs) 277– solar extraterrestrial UV

– ozone layer in the stratosphere 279– spectrum 279

– solar particle events 275– dose equivalent 275– quality factor 275

– survival 145–146radiation dosimetry 314radiative transfer calculations 306radiogenic heating 26816S rDNA sequencing 364recombination 100red dwarf 30 ff.red giant 30 ff., 34, 39reddening 36

reduced chemicals, see also reduction chemistryreduced gradient, see also reduction chemistryreduction chemistry 99redundancy 94regolith 332regulatory proteins 107relicts 103repliaction strategies 103replicase protein 107replication 87, 106–107, 110

– early replication 110– machinery 110– replication strategies 103

Responses of Organisms to the SpaceEnvironment (ROSE) 299–300, 313

return flight 196reverse transcription 105ribonucleic acid 60, see also RNAribonucleotides 64, 105ribose 12, 92, 114ribosomal RNA 109, 112ribosome (ribosomal RNA, NA) 94, 96 ff.,

108–110– proto-ribosome 109–110

ribozymes 13, 87, 108, 111 ff.right-handed (D)-configuration, see also

D-isoform 97RNA 11, 23, 60, 105

– catalytic RNAs 5 ff., 103– mRNA 112– nuclear RNA 112– nucleolar RNA 112– ribosomal RNA, rRNA 109– RNA catalysts 111– RNA enzymes 87, see also ribozymes– RNA genomes 105– RNA interactions 107– RNA-based life 103– rRNA 112– tRNA 110, 112

RNA world 13, 63, 80, 111–115RNA-protein world 108, see also RNP organ-

ismsRNP organisms 106–117rock eaters 161rocket equation 180ff.Rosetta 323, 365Russian satellites 10

ssalt crystals 147sample preparation and distribution system

(SPDS) 344

Index 409

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Saturn 46, 50 ff., 225, 245, 247science fiction 167

– thermosynthetic organisms 169Search for Extraterristrial Intelligence

160seasons (of Titan) 227secretion 90sediment 86sedimentary rocks 15, 323self-sustained life 99serpentinization 7SETUP 236sheet structures 5 ff.shorelines 249signal transduction 90signs of life, searching 328simulation experiments 233single-staged rockets 180 ff.Smart-1 365SNC meteorites 15 ff., 294snow line 45–48snowball Earth 157solar activity

– 11-year cycle 276 ff.solar extraterrestrial UV radiation 305Solar system 15, 46, 203, 307

– age 48– formation 44– habitable zone 159, 170

solar UV 304, 306– extraterrestrial 310

solar UV irradiance– biologically effective 307

solvent 90, 247southwest Greenland 15Soyuz 289Soyuz 2 b 337space age 153space environment 305, 308space experiments 10Space Shuttle 306space simulation facilities 274, 308space vacuum 305

– vacuum-induced dehydration 309spacecraft assembly facility 365, 373spacecraft reentry 323 ff.spacecraft system 199Spacelab 281, 303, 306, 309–310, 312Spacelab 1 280spark discharge 7spectra

– IR 231, 236– UV 231, 236

Spirit 16, see also Marsspontaneous generation 1ff.spore photoproduct 311spores 121

– Bacillus subtilis 306, 310, 312– bacterial 309– fungal 309– inactivation probability 312– survival 121

Sputnik 273Standard Mean Ocean Water SMOW 49ff.Stardust 305, 391stars

– formation 28– population 29, 31

stereoisomer 97sterilization 368, 370, 378–380STONE experiments 17, 314

– basalt 294– dolomite 294– exposure experiments 323– Foton 293ff.– Martian meteorites 294– microorganisms 295– simulatd Martian regolith 294

stop codon 94stratosphere 241, 243stratospheric ozone layer 306Strecker, Adolf 65Streptococcus mitis 147, 376stromatolite 172structure and mechanism system 199structure fraction 181subsurface 327, 335 ff.subsurface drill 327, 339 ff.subsystem 199subterranean environment 144, 322sugars

– synthesis 78suit laboratory 384sulfide 305Sun

– formation 44 ff.super giant (star) 30 ff., 40super-rotation 227supernova 34, 39surface metabolism 8surficial biomass 9survival 146 ff.survival in space 309swing-by maneuver 194Synechococcus 309

Index410

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ttectonic activity 330tectonics 86telluric exoplanets 20telomerase 110, 112telomere 103temperature 227

– Earth 156– planetary surface

– feedback effect 157templated polymerization 116templates 115terminal tag 110thermal control system 199thermosphere 241thioesters 8thiols 8tholins 235–236, 244–245threat to astronauts 335threo furanosyl nucleic acid 14thymidine 92thymine 60ff., 92tidal heating 260ff., 268tidal locking 159Titan 18, 50, 223, 261, 307, 324, see also

Cassini-Huygens– Cassini-Huygens 389ff.– chemical modelling 230, 233– surface 224, 241–242, 248

TNA 14, 115trace molecules 304track detectors 311trajectory biasing 359, 376transcription 96 ff.translation 96, 107–108, 110translation machinery 97, 108triple-alpha reaction 32–33triplet 94tRNA 94, 103, 108tropopause 241troposphere 243turgor 90two-body equation 187

uultraviolet (UV) radiation 321, 324 ff.

– UV radiation 116, 322, 323 ff., 333,342

– UV shielding 323– UV source 234– UV-B radiation 306, 314

Universe– age 25

– average density 27– beginning 25– critical density 27– dark energy 27 ff.– dark matter 28– density 27– expansion rate 27– microwave background 27

uracil 60, 92, 114– synthesis 78

Uranus 46, 50uridine 92

vV-SMOW cross reference to SMOW 49velocity change Dv 179ff.Venus 46, 50, 173, 207, 237, 307

– atmospheric CO2 159– cloud layer

– sulfuric acid 170– dead world 171, 388 ff.– greenhouse warming 159– habitability 159

– clouds 169– temperature on the surface 170– VenusExpress 389– volcanism 158

vertical concentration profiles 233Viking 132, 332, 343 ff.Viking 1 16Viking 2 16Viking lander 130–131, 153Viking mission 130viruses 102, 107vis-viva 187ff.volatiles 86volcanism 86, 158Vostok 273Voyager 242, 254

– IRIS 236– spacecraft 18– UVS 236

Voyager 1 226Voyager mission 256, 261

wwater 23 ff., 35, 41, 44, 45, 47–49, 241, 243,

255, 264– activity 143– ice 229, 245–246– liquid 155, 224–225, 246–247

Index 411

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– ocean 223–224, 246– stability of liquid water 159

weathering 86, 158white dwarf 30–34WMAP 27, 53Wçhler, Friedrich 64

xxenon 46

zzircon 46

Index412

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